The Armstrong Flight Research Center is NASA’s primary center for atmospheric flight research and operations, with a vision “to fly what others only imagine.” We believe that flight validation and research is one of the crucial phases within the advancement of any NASA technology, and it is often the barrier to technology utilization by the private sector. We also believe that aerospace technology can be enhanced through flight early in the Technology Readiness Level (TRL) lifecycle. In fact, some research can be done only in flight. The CIF projects are examples of aerospace technologies that are theoretically advantageous but have had little TRL advancement or are at too early of a technology level for support through a NASA mission.
The focus for the program is on validating, developing, and testing new and innovative technologies.
The current technology areas for the projects included:
AFRC is currently looking into following Technical Capability areas (not in any priority order and not all inclusive):
1. Small launch Space Systems
Develop small launch space systems such as horizontal rockets that could launch to orbit small free-flying space platforms (e.g., cuestas, nanosats, picosats).
2. Altitude Compensating Rocket Systems
Design, build, and test altitude compensating rocket systems or sub-systems designed to operate the rocket efficiently across a wide range of altitudes. Subsystems such as Altitude Compensating Nozzles are being considered.
3. Aero Gravity Assist Systems
Design, build, and test an Aerogravity assist system which uses a close approach to the planet, dipping into the atmosphere, so the spacecraft can also use aerodynamic lift to further curve the trajectory.
4. Launch Vehicle and Spacecraft Adaptive Controls
Develop and test adaptive controls architectures specifically tailored for application to launch vehicles. Adaptive Controls for launch vehicles would include unique features of the aerospace vehicle, such as control-structure interaction, propellant slosh, sensor performance, and actuator dynamics. In addition, the analysis, verification, and flight certification framework for the control system must be addressed.
5. Autonomous Systems
AFRC is exploring concepts for advanced autonomous systems and collaborative autonomous operations that could be applied across aerospace vehicles to enhance effectiveness, survivability, and affordability.
6. Autonomy in a Safety Critical Framework
Armstrong Flight Research Center is interested in the flight demonstration of high level autonomy in a safety critical framework with applicability to man-rated air and space vehicles. This high level of autonomy is enabled through the use of multiple sensor platforms and algorithms with high computational demands. Increased computational capability through embedded high performance computing and implementation of resource efficient algorithms is needed to support this integration. Research into embedded high performance computing using multi-core processors, FPGA, GPU, DSP and associated development of toolchains and algorithms targeted to these platforms is needed in order to reduce the Size, Weight, and Power (SWaP) of the flight vehicles..
7. Space Weather Systems
Design, develop, and test measurement systems to provide the capability for on-demand, validated, and archived radiation measurements related to human tissue and avionics silicon upset concerns.
8. Electromagnetically Boosted Rockets
One possible solution is to use an electromagnetic linear motor boost system to supplement the use of first stage booster rockets and rocket clusters. China Lake is currently advocating to NAVAIR to initiate a study of long term capital costs and recurring system operational costs of the use of an electromagnetic linear motor booster system for their rocket sled tracks as compared to the long term operational system costs of moving to a newer line of booster rocket production.
","parentProgram":{"ableToSelect":false,"acronym":"CIF","isActive":true,"description":"
Through the Center Innovation Fund, the Space Technology Mission Directorate allocates a small portion of the NASA workforce and procurement budget to internal research and development to feed early stage innovation in technology and exploration. Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.
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The Armstrong Flight Research Center is NASA’s primary center for atmospheric flight research and operations, with a vision “to fly what others only imagine.” We believe that flight validation and research is one of the crucial phases within the advancement of any NASA technology, and it is often the barrier to technology utilization by the private sector. We also believe that aerospace technology can be enhanced through flight early in the Technology Readiness Level (TRL) lifecycle. In fact, some research can be done only in flight. The CIF projects are examples of aerospace technologies that are theoretically advantageous but have had little TRL advancement or are at too early of a technology level for support through a NASA mission.
The focus for the program is on validating, developing, and testing new and innovative technologies.
The current technology areas for the projects included:
AFRC is currently looking into following Technical Capability areas (not in any priority order and not all inclusive):
1. Small launch Space Systems
Develop small launch space systems such as horizontal rockets that could launch to orbit small free-flying space platforms (e.g., cuestas, nanosats, picosats).
2. Altitude Compensating Rocket Systems
Design, build, and test altitude compensating rocket systems or sub-systems designed to operate the rocket efficiently across a wide range of altitudes. Subsystems such as Altitude Compensating Nozzles are being considered.
3. Aero Gravity Assist Systems
Design, build, and test an Aerogravity assist system which uses a close approach to the planet, dipping into the atmosphere, so the spacecraft can also use aerodynamic lift to further curve the trajectory.
4. Launch Vehicle and Spacecraft Adaptive Controls
Develop and test adaptive controls architectures specifically tailored for application to launch vehicles. Adaptive Controls for launch vehicles would include unique features of the aerospace vehicle, such as control-structure interaction, propellant slosh, sensor performance, and actuator dynamics. In addition, the analysis, verification, and flight certification framework for the control system must be addressed.
5. Autonomous Systems
AFRC is exploring concepts for advanced autonomous systems and collaborative autonomous operations that could be applied across aerospace vehicles to enhance effectiveness, survivability, and affordability.
6. Autonomy in a Safety Critical Framework
Armstrong Flight Research Center is interested in the flight demonstration of high level autonomy in a safety critical framework with applicability to man-rated air and space vehicles. This high level of autonomy is enabled through the use of multiple sensor platforms and algorithms with high computational demands. Increased computational capability through embedded high performance computing and implementation of resource efficient algorithms is needed to support this integration. Research into embedded high performance computing using multi-core processors, FPGA, GPU, DSP and associated development of toolchains and algorithms targeted to these platforms is needed in order to reduce the Size, Weight, and Power (SWaP) of the flight vehicles..
7. Space Weather Systems
Design, develop, and test measurement systems to provide the capability for on-demand, validated, and archived radiation measurements related to human tissue and avionics silicon upset concerns.
8. Electromagnetically Boosted Rockets
One possible solution is to use an electromagnetic linear motor boost system to supplement the use of first stage booster rockets and rocket clusters. China Lake is currently advocating to NAVAIR to initiate a study of long term capital costs and recurring system operational costs of the use of an electromagnetic linear motor booster system for their rocket sled tracks as compared to the long term operational system costs of moving to a newer line of booster rocket production.
","parentProgram":{"ableToSelect":false,"acronym":"CIF","isActive":true,"description":"
Through the Center Innovation Fund, the Space Technology Mission Directorate allocates a small portion of the NASA workforce and procurement budget to internal research and development to feed early stage innovation in technology and exploration. Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.
","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":64,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"stockImageFileId":36643,"title":"Center Innovation Fund","manageGaps":false,"acronymOrTitle":"CIF"},"parentProgramId":64,"programId":161,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36647,"title":"Center Innovation Fund: AFRC CIF","manageGaps":false,"acronymOrTitle":"AFRC CIF"},"description":"Integration onto an F-18 of JPL's collaborative stereo technology for robust passive (vision based) terrain relative navigation based on two non-static cameras. Primary Technical Hurdles:#• Accurate time synchronization of distributed stereo system#• Real-time camera to camera pose estimation and on-board map construction#• Vibration and motion blur analysis for low altitude flight with wing-tip systems","benefits":"Airborne visual measurements could be used to enhance aircraft or spacecraft vehicle visual awareness, as well as a valuable tool during flight research.","releaseStatus":"Released","status":"Completed","destinationType":[],"trlBegin":3,"trlCurrent":5,"trlEnd":5,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":112848,"canUserEdit":false,"firstName":"David","lastName":"Voracek","fullName":"David F Voracek","fullNameInverted":"Voracek, David F","middleInitial":"F","email":"david.f.voracek@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":104,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":159179,"canUserEdit":false,"firstName":"Gary","lastName":"Fleming","fullName":"Gary A Fleming","fullNameInverted":"Fleming, Gary A","middleInitial":"A","email":"gary.a.fleming@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":226,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":233104,"canUserEdit":false,"firstName":"John","lastName":"Nelson","fullName":"John C Nelson","fullNameInverted":"Nelson, John C","middleInitial":"C","email":"john.c.nelson@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":223,"programId":161,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Sep 2018","startDateString":"Oct 2017"},"relatedProjectId":94054,"relatedProject":{"projectId":94054,"title":"F-18 Stereo Vision Data collection - FY17","startDate":"2016-10-01","startYear":2016,"startMonth":10,"endDate":"2017-07-01","endYear":2017,"endMonth":7,"programId":161,"program":{"ableToSelect":false,"acronym":"AFRC CIF","isActive":true,"description":"
The Armstrong Flight Research Center is NASA’s primary center for atmospheric flight research and operations, with a vision “to fly what others only imagine.” We believe that flight validation and research is one of the crucial phases within the advancement of any NASA technology, and it is often the barrier to technology utilization by the private sector. We also believe that aerospace technology can be enhanced through flight early in the Technology Readiness Level (TRL) lifecycle. In fact, some research can be done only in flight. The CIF projects are examples of aerospace technologies that are theoretically advantageous but have had little TRL advancement or are at too early of a technology level for support through a NASA mission.
The focus for the program is on validating, developing, and testing new and innovative technologies.
The current technology areas for the projects included:
AFRC is currently looking into following Technical Capability areas (not in any priority order and not all inclusive):
1. Small launch Space Systems
Develop small launch space systems such as horizontal rockets that could launch to orbit small free-flying space platforms (e.g., cuestas, nanosats, picosats).
2. Altitude Compensating Rocket Systems
Design, build, and test altitude compensating rocket systems or sub-systems designed to operate the rocket efficiently across a wide range of altitudes. Subsystems such as Altitude Compensating Nozzles are being considered.
3. Aero Gravity Assist Systems
Design, build, and test an Aerogravity assist system which uses a close approach to the planet, dipping into the atmosphere, so the spacecraft can also use aerodynamic lift to further curve the trajectory.
4. Launch Vehicle and Spacecraft Adaptive Controls
Develop and test adaptive controls architectures specifically tailored for application to launch vehicles. Adaptive Controls for launch vehicles would include unique features of the aerospace vehicle, such as control-structure interaction, propellant slosh, sensor performance, and actuator dynamics. In addition, the analysis, verification, and flight certification framework for the control system must be addressed.
5. Autonomous Systems
AFRC is exploring concepts for advanced autonomous systems and collaborative autonomous operations that could be applied across aerospace vehicles to enhance effectiveness, survivability, and affordability.
6. Autonomy in a Safety Critical Framework
Armstrong Flight Research Center is interested in the flight demonstration of high level autonomy in a safety critical framework with applicability to man-rated air and space vehicles. This high level of autonomy is enabled through the use of multiple sensor platforms and algorithms with high computational demands. Increased computational capability through embedded high performance computing and implementation of resource efficient algorithms is needed to support this integration. Research into embedded high performance computing using multi-core processors, FPGA, GPU, DSP and associated development of toolchains and algorithms targeted to these platforms is needed in order to reduce the Size, Weight, and Power (SWaP) of the flight vehicles..
7. Space Weather Systems
Design, develop, and test measurement systems to provide the capability for on-demand, validated, and archived radiation measurements related to human tissue and avionics silicon upset concerns.
8. Electromagnetically Boosted Rockets
One possible solution is to use an electromagnetic linear motor boost system to supplement the use of first stage booster rockets and rocket clusters. China Lake is currently advocating to NAVAIR to initiate a study of long term capital costs and recurring system operational costs of the use of an electromagnetic linear motor booster system for their rocket sled tracks as compared to the long term operational system costs of moving to a newer line of booster rocket production.
","parentProgram":{"ableToSelect":false,"acronym":"CIF","isActive":true,"description":"
Through the Center Innovation Fund, the Space Technology Mission Directorate allocates a small portion of the NASA workforce and procurement budget to internal research and development to feed early stage innovation in technology and exploration. Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.
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Technical Approach / Expected Accomplishment:• Use imagery from cameras to provide on-board range maps of terrain• Non-static stereo camera system (wing-tips of aircraft, 2 UAVs as test bed)requires extraction of stereo geometry before applying stereo algorithm• Differential GPS module coupled with each camera to provide distance between cameras and precision time synchronization• Prove of concept on JPL tandem UAV system• Evaluate quality of 3D reconstruction for terrain relative navigation (TRN)and collision avoidance at low altitudes on AFRC fixed-wing aircraft (8ftDROID UAV, AFRC F18 test aircraft - leveraging regular training flights)
","benefits":"Primary Technical Hurdles:• Accurate time synchronization of distributed stereo system• Real-time camera to camera pose estimation and on-board map construction• Vibration and motion blur analysis for low altitude flight with wing-tip systems
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The focus for the program is on validating, developing, and testing new and innovative technologies.
The current technology areas for the projects included:
AFRC is currently looking into following Technical Capability areas (not in any priority order and not all inclusive):
1. Small launch Space Systems
Develop small launch space systems such as horizontal rockets that could launch to orbit small free-flying space platforms (e.g., cuestas, nanosats, picosats).
2. Altitude Compensating Rocket Systems
Design, build, and test altitude compensating rocket systems or sub-systems designed to operate the rocket efficiently across a wide range of altitudes. Subsystems such as Altitude Compensating Nozzles are being considered.
3. Aero Gravity Assist Systems
Design, build, and test an Aerogravity assist system which uses a close approach to the planet, dipping into the atmosphere, so the spacecraft can also use aerodynamic lift to further curve the trajectory.
4. Launch Vehicle and Spacecraft Adaptive Controls
Develop and test adaptive controls architectures specifically tailored for application to launch vehicles. Adaptive Controls for launch vehicles would include unique features of the aerospace vehicle, such as control-structure interaction, propellant slosh, sensor performance, and actuator dynamics. In addition, the analysis, verification, and flight certification framework for the control system must be addressed.
5. Autonomous Systems
AFRC is exploring concepts for advanced autonomous systems and collaborative autonomous operations that could be applied across aerospace vehicles to enhance effectiveness, survivability, and affordability.
6. Autonomy in a Safety Critical Framework
Armstrong Flight Research Center is interested in the flight demonstration of high level autonomy in a safety critical framework with applicability to man-rated air and space vehicles. This high level of autonomy is enabled through the use of multiple sensor platforms and algorithms with high computational demands. Increased computational capability through embedded high performance computing and implementation of resource efficient algorithms is needed to support this integration. Research into embedded high performance computing using multi-core processors, FPGA, GPU, DSP and associated development of toolchains and algorithms targeted to these platforms is needed in order to reduce the Size, Weight, and Power (SWaP) of the flight vehicles..
7. Space Weather Systems
Design, develop, and test measurement systems to provide the capability for on-demand, validated, and archived radiation measurements related to human tissue and avionics silicon upset concerns.
8. Electromagnetically Boosted Rockets
One possible solution is to use an electromagnetic linear motor boost system to supplement the use of first stage booster rockets and rocket clusters. China Lake is currently advocating to NAVAIR to initiate a study of long term capital costs and recurring system operational costs of the use of an electromagnetic linear motor booster system for their rocket sled tracks as compared to the long term operational system costs of moving to a newer line of booster rocket production.
","parentProgram":{"ableToSelect":false,"acronym":"CIF","isActive":true,"description":"
Through the Center Innovation Fund, the Space Technology Mission Directorate allocates a small portion of the NASA workforce and procurement budget to internal research and development to feed early stage innovation in technology and exploration. Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.
","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":64,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"stockImageFileId":36643,"title":"Center Innovation Fund","manageGaps":false,"acronymOrTitle":"CIF"},"parentProgramId":64,"programId":161,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36647,"title":"Center Innovation Fund: AFRC CIF","manageGaps":false,"acronymOrTitle":"AFRC CIF"},"description":"Integration onto an F-18 of JPL's collaborative stereo technology for robust passive (vision based) terrain relative navigation based on two non-static cameras. Primary Technical Hurdles:#• Accurate time synchronization of distributed stereo system#• Real-time camera to camera pose estimation and on-board map construction#• Vibration and motion blur analysis for low altitude flight with wing-tip systems","benefits":"Airborne visual measurements could be used to enhance aircraft or spacecraft vehicle visual awareness, as well as a valuable tool during flight research.","releaseStatus":"Released","status":"Completed","destinationType":[],"trlBegin":3,"trlCurrent":5,"trlEnd":5,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":112848,"canUserEdit":false,"firstName":"David","lastName":"Voracek","fullName":"David F Voracek","fullNameInverted":"Voracek, David F","middleInitial":"F","email":"david.f.voracek@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":104,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":159179,"canUserEdit":false,"firstName":"Gary","lastName":"Fleming","fullName":"Gary A Fleming","fullNameInverted":"Fleming, Gary A","middleInitial":"A","email":"gary.a.fleming@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":226,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":233104,"canUserEdit":false,"firstName":"John","lastName":"Nelson","fullName":"John C Nelson","fullNameInverted":"Nelson, John C","middleInitial":"C","email":"john.c.nelson@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":223,"programId":161,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Sep 2018","startDateString":"Oct 2017"},"technologyOutcomePartner":"Other_NASA_Program_or_Directorate","technologyOutcomeDate":"2018-09-30","technologyOutcomePath":"Transitioned_To","details":"NASA Armstrong \"Resilient Autonomy\"","infoText":"Transitioned To Other NASA Program or Directorate","infoTextExtra":"Other NASA Program or Directorate","isIndirect":false,"infusionPretty":"","isBiDirectional":false,"technologyOutcomeDateString":"Sep 2018","technologyOutcomeDateFullString":"September 2018","technologyOutcomePartnerPretty":"Other NASA Program or Directorate","technologyOutcomePathPretty":"Transitioned To","technologyOutcomeRationalePretty":""},{"technologyOutcomeId":97668,"projectId":94001,"project":{"projectId":94001,"title":"F-18 Stereo Vision Data collection - FY18","startDate":"2017-10-01","startYear":2017,"startMonth":10,"endDate":"2018-09-30","endYear":2018,"endMonth":9,"programId":161,"program":{"ableToSelect":false,"acronym":"AFRC CIF","isActive":true,"description":"
The Armstrong Flight Research Center is NASA’s primary center for atmospheric flight research and operations, with a vision “to fly what others only imagine.” We believe that flight validation and research is one of the crucial phases within the advancement of any NASA technology, and it is often the barrier to technology utilization by the private sector. We also believe that aerospace technology can be enhanced through flight early in the Technology Readiness Level (TRL) lifecycle. In fact, some research can be done only in flight. The CIF projects are examples of aerospace technologies that are theoretically advantageous but have had little TRL advancement or are at too early of a technology level for support through a NASA mission.
The focus for the program is on validating, developing, and testing new and innovative technologies.
The current technology areas for the projects included:
AFRC is currently looking into following Technical Capability areas (not in any priority order and not all inclusive):
1. Small launch Space Systems
Develop small launch space systems such as horizontal rockets that could launch to orbit small free-flying space platforms (e.g., cuestas, nanosats, picosats).
2. Altitude Compensating Rocket Systems
Design, build, and test altitude compensating rocket systems or sub-systems designed to operate the rocket efficiently across a wide range of altitudes. Subsystems such as Altitude Compensating Nozzles are being considered.
3. Aero Gravity Assist Systems
Design, build, and test an Aerogravity assist system which uses a close approach to the planet, dipping into the atmosphere, so the spacecraft can also use aerodynamic lift to further curve the trajectory.
4. Launch Vehicle and Spacecraft Adaptive Controls
Develop and test adaptive controls architectures specifically tailored for application to launch vehicles. Adaptive Controls for launch vehicles would include unique features of the aerospace vehicle, such as control-structure interaction, propellant slosh, sensor performance, and actuator dynamics. In addition, the analysis, verification, and flight certification framework for the control system must be addressed.
5. Autonomous Systems
AFRC is exploring concepts for advanced autonomous systems and collaborative autonomous operations that could be applied across aerospace vehicles to enhance effectiveness, survivability, and affordability.
6. Autonomy in a Safety Critical Framework
Armstrong Flight Research Center is interested in the flight demonstration of high level autonomy in a safety critical framework with applicability to man-rated air and space vehicles. This high level of autonomy is enabled through the use of multiple sensor platforms and algorithms with high computational demands. Increased computational capability through embedded high performance computing and implementation of resource efficient algorithms is needed to support this integration. Research into embedded high performance computing using multi-core processors, FPGA, GPU, DSP and associated development of toolchains and algorithms targeted to these platforms is needed in order to reduce the Size, Weight, and Power (SWaP) of the flight vehicles..
7. Space Weather Systems
Design, develop, and test measurement systems to provide the capability for on-demand, validated, and archived radiation measurements related to human tissue and avionics silicon upset concerns.
8. Electromagnetically Boosted Rockets
One possible solution is to use an electromagnetic linear motor boost system to supplement the use of first stage booster rockets and rocket clusters. China Lake is currently advocating to NAVAIR to initiate a study of long term capital costs and recurring system operational costs of the use of an electromagnetic linear motor booster system for their rocket sled tracks as compared to the long term operational system costs of moving to a newer line of booster rocket production.
","parentProgram":{"ableToSelect":false,"acronym":"CIF","isActive":true,"description":"
Through the Center Innovation Fund, the Space Technology Mission Directorate allocates a small portion of the NASA workforce and procurement budget to internal research and development to feed early stage innovation in technology and exploration. Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.
","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":64,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"stockImageFileId":36643,"title":"Center Innovation Fund","manageGaps":false,"acronymOrTitle":"CIF"},"parentProgramId":64,"programId":161,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36647,"title":"Center Innovation Fund: AFRC CIF","manageGaps":false,"acronymOrTitle":"AFRC CIF"},"description":"Integration onto an F-18 of JPL's collaborative stereo technology for robust passive (vision based) terrain relative navigation based on two non-static cameras. Primary Technical Hurdles:#• Accurate time synchronization of distributed stereo system#• Real-time camera to camera pose estimation and on-board map construction#• Vibration and motion blur analysis for low altitude flight with wing-tip systems","benefits":"Airborne visual measurements could be used to enhance aircraft or spacecraft vehicle visual awareness, as well as a valuable tool during flight research.","releaseStatus":"Released","status":"Completed","destinationType":[],"trlBegin":3,"trlCurrent":5,"trlEnd":5,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":112848,"canUserEdit":false,"firstName":"David","lastName":"Voracek","fullName":"David F Voracek","fullNameInverted":"Voracek, David F","middleInitial":"F","email":"david.f.voracek@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":104,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":159179,"canUserEdit":false,"firstName":"Gary","lastName":"Fleming","fullName":"Gary A Fleming","fullNameInverted":"Fleming, Gary A","middleInitial":"A","email":"gary.a.fleming@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":226,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":233104,"canUserEdit":false,"firstName":"John","lastName":"Nelson","fullName":"John C Nelson","fullNameInverted":"Nelson, John C","middleInitial":"C","email":"john.c.nelson@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":223,"programId":161,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Sep 2018","startDateString":"Oct 2017"},"technologyOutcomeDate":"2018-09-30","technologyOutcomePath":"Closed_Out","details":"We expect to complete two flights with the camera pods In February 2019. This will enable JPL to take the initial data and make decisions about how to move forward with this innovation.","infoText":"Closed out","infoTextExtra":"Project closed out","isIndirect":false,"infusionPretty":"","isBiDirectional":false,"technologyOutcomeDateString":"Sep 2018","technologyOutcomeDateFullString":"September 2018","technologyOutcomePartnerPretty":"","technologyOutcomePathPretty":"Closed Out","technologyOutcomeRationalePretty":""},{"technologyOutcomeId":97726,"projectId":94001,"project":{"projectId":94001,"title":"F-18 Stereo Vision Data collection - FY18","startDate":"2017-10-01","startYear":2017,"startMonth":10,"endDate":"2018-09-30","endYear":2018,"endMonth":9,"programId":161,"program":{"ableToSelect":false,"acronym":"AFRC CIF","isActive":true,"description":"
The Armstrong Flight Research Center is NASA’s primary center for atmospheric flight research and operations, with a vision “to fly what others only imagine.” We believe that flight validation and research is one of the crucial phases within the advancement of any NASA technology, and it is often the barrier to technology utilization by the private sector. We also believe that aerospace technology can be enhanced through flight early in the Technology Readiness Level (TRL) lifecycle. In fact, some research can be done only in flight. The CIF projects are examples of aerospace technologies that are theoretically advantageous but have had little TRL advancement or are at too early of a technology level for support through a NASA mission.
The focus for the program is on validating, developing, and testing new and innovative technologies.
The current technology areas for the projects included:
AFRC is currently looking into following Technical Capability areas (not in any priority order and not all inclusive):
1. Small launch Space Systems
Develop small launch space systems such as horizontal rockets that could launch to orbit small free-flying space platforms (e.g., cuestas, nanosats, picosats).
2. Altitude Compensating Rocket Systems
Design, build, and test altitude compensating rocket systems or sub-systems designed to operate the rocket efficiently across a wide range of altitudes. Subsystems such as Altitude Compensating Nozzles are being considered.
3. Aero Gravity Assist Systems
Design, build, and test an Aerogravity assist system which uses a close approach to the planet, dipping into the atmosphere, so the spacecraft can also use aerodynamic lift to further curve the trajectory.
4. Launch Vehicle and Spacecraft Adaptive Controls
Develop and test adaptive controls architectures specifically tailored for application to launch vehicles. Adaptive Controls for launch vehicles would include unique features of the aerospace vehicle, such as control-structure interaction, propellant slosh, sensor performance, and actuator dynamics. In addition, the analysis, verification, and flight certification framework for the control system must be addressed.
5. Autonomous Systems
AFRC is exploring concepts for advanced autonomous systems and collaborative autonomous operations that could be applied across aerospace vehicles to enhance effectiveness, survivability, and affordability.
6. Autonomy in a Safety Critical Framework
Armstrong Flight Research Center is interested in the flight demonstration of high level autonomy in a safety critical framework with applicability to man-rated air and space vehicles. This high level of autonomy is enabled through the use of multiple sensor platforms and algorithms with high computational demands. Increased computational capability through embedded high performance computing and implementation of resource efficient algorithms is needed to support this integration. Research into embedded high performance computing using multi-core processors, FPGA, GPU, DSP and associated development of toolchains and algorithms targeted to these platforms is needed in order to reduce the Size, Weight, and Power (SWaP) of the flight vehicles..
7. Space Weather Systems
Design, develop, and test measurement systems to provide the capability for on-demand, validated, and archived radiation measurements related to human tissue and avionics silicon upset concerns.
8. Electromagnetically Boosted Rockets
One possible solution is to use an electromagnetic linear motor boost system to supplement the use of first stage booster rockets and rocket clusters. China Lake is currently advocating to NAVAIR to initiate a study of long term capital costs and recurring system operational costs of the use of an electromagnetic linear motor booster system for their rocket sled tracks as compared to the long term operational system costs of moving to a newer line of booster rocket production.
","parentProgram":{"ableToSelect":false,"acronym":"CIF","isActive":true,"description":"
Through the Center Innovation Fund, the Space Technology Mission Directorate allocates a small portion of the NASA workforce and procurement budget to internal research and development to feed early stage innovation in technology and exploration. Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.
","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":64,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"stockImageFileId":36643,"title":"Center Innovation Fund","manageGaps":false,"acronymOrTitle":"CIF"},"parentProgramId":64,"programId":161,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36647,"title":"Center Innovation Fund: AFRC CIF","manageGaps":false,"acronymOrTitle":"AFRC CIF"},"description":"Integration onto an F-18 of JPL's collaborative stereo technology for robust passive (vision based) terrain relative navigation based on two non-static cameras. Primary Technical Hurdles:#• Accurate time synchronization of distributed stereo system#• Real-time camera to camera pose estimation and on-board map construction#• Vibration and motion blur analysis for low altitude flight with wing-tip systems","benefits":"Airborne visual measurements could be used to enhance aircraft or spacecraft vehicle visual awareness, as well as a valuable tool during flight research.","releaseStatus":"Released","status":"Completed","destinationType":[],"trlBegin":3,"trlCurrent":5,"trlEnd":5,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":112848,"canUserEdit":false,"firstName":"David","lastName":"Voracek","fullName":"David F Voracek","fullNameInverted":"Voracek, David F","middleInitial":"F","email":"david.f.voracek@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":104,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":159179,"canUserEdit":false,"firstName":"Gary","lastName":"Fleming","fullName":"Gary A Fleming","fullNameInverted":"Fleming, Gary A","middleInitial":"A","email":"gary.a.fleming@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":226,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":233104,"canUserEdit":false,"firstName":"John","lastName":"Nelson","fullName":"John C Nelson","fullNameInverted":"Nelson, John C","middleInitial":"C","email":"john.c.nelson@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":223,"programId":161,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Sep 2018","startDateString":"Oct 2017"},"relatedProjectId":94054,"relatedProject":{"projectId":94054,"title":"F-18 Stereo Vision Data collection - FY17","startDate":"2016-10-01","startYear":2016,"startMonth":10,"endDate":"2017-07-01","endYear":2017,"endMonth":7,"programId":161,"program":{"ableToSelect":false,"acronym":"AFRC CIF","isActive":true,"description":"
The Armstrong Flight Research Center is NASA’s primary center for atmospheric flight research and operations, with a vision “to fly what others only imagine.” We believe that flight validation and research is one of the crucial phases within the advancement of any NASA technology, and it is often the barrier to technology utilization by the private sector. We also believe that aerospace technology can be enhanced through flight early in the Technology Readiness Level (TRL) lifecycle. In fact, some research can be done only in flight. The CIF projects are examples of aerospace technologies that are theoretically advantageous but have had little TRL advancement or are at too early of a technology level for support through a NASA mission.
The focus for the program is on validating, developing, and testing new and innovative technologies.
The current technology areas for the projects included:
AFRC is currently looking into following Technical Capability areas (not in any priority order and not all inclusive):
1. Small launch Space Systems
Develop small launch space systems such as horizontal rockets that could launch to orbit small free-flying space platforms (e.g., cuestas, nanosats, picosats).
2. Altitude Compensating Rocket Systems
Design, build, and test altitude compensating rocket systems or sub-systems designed to operate the rocket efficiently across a wide range of altitudes. Subsystems such as Altitude Compensating Nozzles are being considered.
3. Aero Gravity Assist Systems
Design, build, and test an Aerogravity assist system which uses a close approach to the planet, dipping into the atmosphere, so the spacecraft can also use aerodynamic lift to further curve the trajectory.
4. Launch Vehicle and Spacecraft Adaptive Controls
Develop and test adaptive controls architectures specifically tailored for application to launch vehicles. Adaptive Controls for launch vehicles would include unique features of the aerospace vehicle, such as control-structure interaction, propellant slosh, sensor performance, and actuator dynamics. In addition, the analysis, verification, and flight certification framework for the control system must be addressed.
5. Autonomous Systems
AFRC is exploring concepts for advanced autonomous systems and collaborative autonomous operations that could be applied across aerospace vehicles to enhance effectiveness, survivability, and affordability.
6. Autonomy in a Safety Critical Framework
Armstrong Flight Research Center is interested in the flight demonstration of high level autonomy in a safety critical framework with applicability to man-rated air and space vehicles. This high level of autonomy is enabled through the use of multiple sensor platforms and algorithms with high computational demands. Increased computational capability through embedded high performance computing and implementation of resource efficient algorithms is needed to support this integration. Research into embedded high performance computing using multi-core processors, FPGA, GPU, DSP and associated development of toolchains and algorithms targeted to these platforms is needed in order to reduce the Size, Weight, and Power (SWaP) of the flight vehicles..
7. Space Weather Systems
Design, develop, and test measurement systems to provide the capability for on-demand, validated, and archived radiation measurements related to human tissue and avionics silicon upset concerns.
8. Electromagnetically Boosted Rockets
One possible solution is to use an electromagnetic linear motor boost system to supplement the use of first stage booster rockets and rocket clusters. China Lake is currently advocating to NAVAIR to initiate a study of long term capital costs and recurring system operational costs of the use of an electromagnetic linear motor booster system for their rocket sled tracks as compared to the long term operational system costs of moving to a newer line of booster rocket production.
","parentProgram":{"ableToSelect":false,"acronym":"CIF","isActive":true,"description":"
Through the Center Innovation Fund, the Space Technology Mission Directorate allocates a small portion of the NASA workforce and procurement budget to internal research and development to feed early stage innovation in technology and exploration. Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.
","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":64,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"stockImageFileId":36643,"title":"Center Innovation Fund","manageGaps":false,"acronymOrTitle":"CIF"},"parentProgramId":64,"programId":161,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36647,"title":"Center Innovation Fund: AFRC CIF","manageGaps":false,"acronymOrTitle":"AFRC CIF"},"description":"
Technical Approach / Expected Accomplishment:• Use imagery from cameras to provide on-board range maps of terrain• Non-static stereo camera system (wing-tips of aircraft, 2 UAVs as test bed)requires extraction of stereo geometry before applying stereo algorithm• Differential GPS module coupled with each camera to provide distance between cameras and precision time synchronization• Prove of concept on JPL tandem UAV system• Evaluate quality of 3D reconstruction for terrain relative navigation (TRN)and collision avoidance at low altitudes on AFRC fixed-wing aircraft (8ftDROID UAV, AFRC F18 test aircraft - leveraging regular training flights)
","benefits":"Primary Technical Hurdles:• Accurate time synchronization of distributed stereo system• Real-time camera to camera pose estimation and on-board map construction• Vibration and motion blur analysis for low altitude flight with wing-tip systems
","releaseStatus":"Released","status":"Completed","destinationType":[],"trlBegin":2,"trlCurrent":3,"trlEnd":3,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":112848,"canUserEdit":false,"firstName":"David","lastName":"Voracek","fullName":"David F Voracek","fullNameInverted":"Voracek, David F","middleInitial":"F","email":"david.f.voracek@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":104,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":159179,"canUserEdit":false,"firstName":"Gary","lastName":"Fleming","fullName":"Gary A Fleming","fullNameInverted":"Fleming, Gary A","middleInitial":"A","email":"gary.a.fleming@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":226,"programId":161,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":233104,"canUserEdit":false,"firstName":"John","lastName":"Nelson","fullName":"John C Nelson","fullNameInverted":"Nelson, John C","middleInitial":"C","email":"john.c.nelson@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":223,"programId":161,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Jul 2017","startDateString":"Oct 2016"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2017-10-01","technologyOutcomePath":"Advanced_From","infoText":"Advanced from another project within the program","infoTextExtra":"Another project within the program (F-18 Stereo Vision Data collection - FY17)","isIndirect":true,"infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateString":"Oct 2017","technologyOutcomeDateFullString":"October 2017","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced From","technologyOutcomeRationalePretty":""}],"libraryItems":[{"files":[],"libraryItemId":367906,"title":"Project Website","libraryItemType":"Link","url":"https://www.nasa.gov/directorates/spacetech/innovation_fund/index.html#.VQb6gUjJzyE","projectId":94001,"internalOnly":false,"publishedDateString":"","entryDateString":"01/22/25 01:10 AM","libraryItemTypePretty":"Link","modifiedDateString":"10/25/24 02:23 PM"}],"states":[{"abbreviation":"CA","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"California","stateTerritoryId":59,"isTerritory":false}],"endDateString":"Sep 2018","startDateString":"Oct 2017"}}