{"projectId":14742,"project":{"projectId":14742,"title":"Active Collision Avoidance for Planetary Landers","startDate":"2013-10-01","startYear":2013,"startMonth":10,"endDate":"2014-09-30","endYear":2014,"endMonth":9,"programId":168,"program":{"ableToSelect":false,"acronym":"MSFC 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,"acronym":"CIF","isActive":true,"description":"<p>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.&nbsp;Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. &nbsp;These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.</p><p>&nbsp;</p><p>&nbsp;</p>","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":168,"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":36644,"title":"Center Innovation Fund: MSFC CIF","manageGaps":false,"acronymOrTitle":"MSFC CIF"},"description":"Present day robotic missions to other planets require precise, a priori knowledge of the terrain to pre-determine a landing spot that is safe. Landing sites can be miles from the mission objective, or, mission objectives may be tailored to suit landing sites. Future robotic exploration missions should be capable of autonomously identifying a safe landing target within a specified target area selected by mission requirements. Such autonomous landing systems must (1) 'see' the surface, (2) identify a target, and (3) land the vehicle. Recent advances in radar technology have resulted in small, lightweight, low power radars that are used for collision avoidance and cruise control systems in automobiles. Such radar systems can be adapted for use as active hazard avoidance systems for planetary landers. The focus of this CIF proposal is to leverage earlier work on collision avoidance systems for MSFC's Mighty Eagle lander and evaluate the use of automotive radar systems for collision avoidance in planetary landers. Advancements in radar technology have resulted in commercial, automotive collision avoidance radars. These radar systems typically use 37GHz or 77GHz interferometry to identify hazards around a vehicle. This is done by developing a high-resolution 'topographic' map of the area surrounding the vehicle and identifying potential changes in the surrounding area. The technology should not be confused with older radar systems, which do not use interferometry. Automotive interferometric systems are designed to be lightweight, consume little electric power, and are small enough to fit into fenders of vehicles. These systems have enormous potential in performing the same functions for planetary landers. Compared to systems dependent on optical wavelengths, suspended dust, small particles and aerosols are transparent to radar's much longer wavelengths. The automotive collision avoidance systems are not inhibited by dust clouds as are optical systems, are relatively small, and do not consume much power – three key characteristics that make them good candidates for a collision avoidance system. Radar systems, from vendors like Delphi Automotive, are available with the full complement of hardware, processing software and visualization systems. We emphasize the importance of the existing software base. Replicating the investment represented by these packages is prohibitive. Freescale Semiconductors, an industry leader in advanced integrated circuits, have recently announced the availability of a single chip automotive radar solution at different frequencies. These single-chip solutions are state-of-the-art technologies that integrate the entire front-end of a radar system into a single surface mount device, that occupies less that 1 sq. cm. This product significantly miniaturizes a potential collision avoidance system. However, these radars are calibrated for use in an automotive application. Radar reflectivity and target detection is based on known radar cross sections for typical vehicular use. In our effort, we will evaluate a Delphi or similar radar solution for MSFC's Mighty Eagle and Lunar Surface Testbed. In the first year evaluation will with a static platform. The evaluation will consist of understanding the radar signature (at automotive radar frequencies) of a simulated lunar surface and also evaluate the performance of the built-in target detection capability of a COTS radar system. In addition, we will begin evaluation of the Freescale Semiconductor solution. This will enhance our in-house capability to design and build our own system that will incorporate the knowledge gained from using the Delphi system in the terrain field. There are several significant elements in the evaluation. Here we specifically note the following to give some indication of the range and nature of the elements. (1) What interference to other spacecraft systems might happen? (2) How does placement on the spacecraft affect the performance of the radar? (3) What is the distance-object size-surface morphology-particle size-particle shape-particle composition detectability performance? (4) How sensitive are the tests to moisture in the simulant? The later point is a practical concern that must be addressed in order to evaluate the other elements. We are aware that rocket exhaust can interfere with radar frequencies. The significant of this effect at the target wavelengths with our instrument/lander geometry for an interferometric system will be evaluated.","benefits":"<p>Hazard Avoidance is one of the great technical challenges for autonomous missions to planetary objectives of high scientific interest (inside craters or near outcrops for example). The importance of this problem is well known and validated by the Agency's investment in systems such as ALHAT. For appropriate mission profiles the proposed radar system is thought to be less expensive, lower weight, use less electric power, and to be more technically capable than systems such as the LIDAR system considered for ALHAT. These considerations are vital for small, low cost missions.</p>","releaseStatus":"Released","status":"Completed","viewCount":651,"destinationType":[],"trlBegin":2,"trlCurrent":3,"trlEnd":3,"lastUpdated":"12/18/25","favorited":false,"detailedFunding":false,"projectContacts":[{"contactId":127976,"canUserEdit":false,"firstName":"Doug","lastName":"Rickman","fullName":"Doug Rickman","fullNameInverted":"Rickman, Doug","email":"Douglas.L.Rickman@nasa.gov","receiveEmail":"Subscribed_User","projectContactRole":"Principal_Investigator","projectContactId":541717,"projectId":14742,"programContactRolePretty":"","projectContactRolePretty":"Principal Investigator"}],"programContacts":[],"leadOrganization":{"organizationId":4854,"organizationName":"Marshall Space Flight Center","acronym":"MSFC","organizationType":"NASA_Center","city":"Huntsville","stateTerritoryId":18,"stateTerritory":{"abbreviation":"AL","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Alabama","stateTerritoryId":18,"isTerritory":false},"country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"zipCode":"35812","projectId":14742,"projectOrganizationId":569645,"organizationRole":"Lead_Organization","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"Lead Organization","organizationTypePretty":"NASA Center"},"otherOrganizations":[{"organizationId":4854,"organizationName":"Marshall Space Flight Center","acronym":"MSFC","organizationType":"NASA_Center","city":"Huntsville","stateTerritoryId":18,"stateTerritory":{"abbreviation":"AL","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Alabama","stateTerritoryId":18,"isTerritory":false},"country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"zipCode":"35812","projectId":14742,"projectOrganizationId":569645,"organizationRole":"Lead_Organization","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"Lead Organization","organizationTypePretty":"NASA Center"}],"primaryTx":{"taxonomyNodeId":11220,"taxonomyRootId":8817,"parentNodeId":11216,"code":"TX08.1.4","title":"Microwave, Millimeter Waves, and Submillimeter Waves","description":"Microwave and radio transmitter and receiver component technologies for the 30 kHz to 10 THz range include integrated radar transmitter/receiver (T/R) modules and integrated radiometer receivers, active microwave instruments (radar), passive radiometers (microwave and far infrared), and crosscutting technologies such as radiation-hardened electronics.","exampleTechnologies":"Laser heterodyne and gas correlation radiometers, low noise receivers, transmit/receive modules, couplers/combiners, isolators, amplifiers, filters, antennas, waveguide components","level":3,"hasChildren":false,"selected":false,"isPrimary":true,"hasInteriorContent":true},"primaryTxTree":[[{"taxonomyNodeId":11215,"taxonomyRootId":8817,"code":"TX08","title":"Sensors and Instruments","level":1,"hasChildren":true,"selected":false,"hasInteriorContent":true},{"taxonomyNodeId":11216,"taxonomyRootId":8817,"parentNodeId":11215,"code":"TX08.1","title":"Remote Sensing Instruments and Sensors","description":"Remote sensing instruments and sensors include components, sensors, and instruments that are sensitive to electromagnetic radiation; particles (charged, neutral, dust); electromagnetic fields, both direct current (DC) and alternating current (AC); acoustic energy; seismic energy; and whatever physical phenomenology the science requires. 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These radar systems typically use 37GHz or 77GHz interferometry to identify hazards around a vehicle. This is done by developing a high-resolution 'topographic' map of the area surrounding the vehicle and identifying potential changes in the surrounding area. The technology should not be confused with older radar systems, which do not use interferometry. Automotive interferometric systems are designed to be lightweight, consume little electric power, and are small enough to fit into fenders of vehicles. These systems have enormous potential in performing the same functions for planetary landers. Compared to systems dependent on optical wavelengths, suspended dust, small particles and aerosols are transparent to radar's much longer wavelengths. The automotive collision avoidance systems are not inhibited by dust clouds as are optical systems, are relatively small, and do not consume much power – three key characteristics that make them good candidates for a collision avoidance system. Radar systems, from vendors like Delphi Automotive, are available with the full complement of hardware, processing software and visualization systems. We emphasize the importance of the existing software base. Replicating the investment represented by these packages is prohibitive. Freescale Semiconductors, an industry leader in advanced integrated circuits, have recently announced the availability of a single chip automotive radar solution at different frequencies. These single-chip solutions are state-of-the-art technologies that integrate the entire front-end of a radar system into a single surface mount device, that occupies less that 1 sq. cm. This product significantly miniaturizes a potential collision avoidance system. However, these radars are calibrated for use in an automotive application. Radar reflectivity and target detection is based on known radar cross sections for typical vehicular use. In our effort, we will evaluate a Delphi or similar radar solution for MSFC's Mighty Eagle and Lunar Surface Testbed. In the first year evaluation will with a static platform. The evaluation will consist of understanding the radar signature (at automotive radar frequencies) of a simulated lunar surface and also evaluate the performance of the built-in target detection capability of a COTS radar system. In addition, we will begin evaluation of the Freescale Semiconductor solution. This will enhance our in-house capability to design and build our own system that will incorporate the knowledge gained from using the Delphi system in the terrain field. There are several significant elements in the evaluation. Here we specifically note the following to give some indication of the range and nature of the elements. (1) What interference to other spacecraft systems might happen? (2) How does placement on the spacecraft affect the performance of the radar? (3) What is the distance-object size-surface morphology-particle size-particle shape-particle composition detectability performance? (4) How sensitive are the tests to moisture in the simulant? The later point is a practical concern that must be addressed in order to evaluate the other elements. We are aware that rocket exhaust can interfere with radar frequencies. The significant of this effect at the target wavelengths with our instrument/lander geometry for an interferometric system will be evaluated.","benefits":"<p>Hazard Avoidance is one of the great technical challenges for autonomous missions to planetary objectives of high scientific interest (inside craters or near outcrops for example). The importance of this problem is well known and validated by the Agency's investment in systems such as ALHAT. For appropriate mission profiles the proposed radar system is thought to be less expensive, lower weight, use less electric power, and to be more technically capable than systems such as the LIDAR system considered for ALHAT. These considerations are vital for small, low cost missions.</p>","releaseStatus":"Released","status":"Completed","destinationType":[],"trlBegin":2,"trlCurrent":3,"trlEnd":3,"favorited":false,"detailedFunding":false,"programContacts":[],"endDateString":"Sep 2014","startDateString":"Oct 2013"},"relatedProjectId":23351,"relatedProject":{"projectId":23351,"title":"Radar Hazard Identification for Planetary Landers D Stage 2","startDate":"2014-11-01","startYear":2014,"startMonth":11,"endDate":"2015-10-01","endYear":2015,"endMonth":10,"programId":168,"program":{"ableToSelect":false,"acronym":"MSFC 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,"acronym":"CIF","isActive":true,"description":"<p>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.&nbsp;Activities with in the Center Innovation Fund are proposed and led by NASA scientists and engineers. &nbsp;These activities and creative initiatives pursue emerging technologies that leverage talent and capabilities at the NASA Centers.</p><p>&nbsp;</p><p>&nbsp;</p>","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":168,"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":36644,"title":"Center Innovation Fund: MSFC CIF","manageGaps":false,"acronymOrTitle":"MSFC CIF"},"description":"<p>Present day robotic missions to other planets require extensive knowledge of the terrain in order to pre-determine a landing zone that is relatively devoid of hazards. Without hazard avoidance systems mission planners have to compromise on scientific objectives for a safe landing site. Future robotic exploration missions should be capable of autonomously identifying a safe landing target within a specified target area selected by mission requirements. Recent advances in radar technology have resulted in small, lightweight, low power radars that are used for collision avoidance and cruise control systems in automobiles. Such radar systems warrant testing for use in hazard avoidance systems for planetary landers. This CIF proposal seeks to complete the evaluation and characterization of an automotive radar system in the MSFC lunar terrain field under various simulated robotic lander descent profiles. NASA Headquarters chartered the Autonomous Precision Landing and Hazard Avoidance Technology (ALHAT) project in 2005 to enable precision landing at any site under any lighting conditions. In 2014 ALHAT conducted a series of flight tests aboard the Morpheus vertical testbed at the KSC terrain field. One of the findings of the Morpheus/ALHAT tests is lidar-based systems struggle when moving dust and/or rocket exhaust is between the sensor and the target being mapped. The same phenomena was also observed with the Mighty Eagle testing of a stereo camera for hazard avoidance. Rocky planetary surfaces are dusty; hazard detection systems must deal with dust on close approach. The proposed activity continues a FY2014 CIF project. The two-year activity seeks to test a commercial, automotive interferometric radar for detection of hazards by autonomous landers. Advancement in radar and computer technologies has resulted in such radars being used in many vehicles. These interferometric radar systems typically use 37GHz or 77GHz to identify hazards around a vehicle. The systems are lightweight, low power, and small enough to fit into a vehicle's fender. The signal processing capabilities integral to the automotive units fundamentally change the cost/performance relationships normally associated with the aerospace uses of radar. These automotive systems have enormous potential to perform an analogous function for planetary landers. Further, compared to systems dependent on optical wavelengths, suspended dust, small particles and aerosols are transparent to these radar's much longer wavelengths. In Year 1 we procured a radar, developed a portable data acquisition system, wrote software to handle the data, and tested the unit in multiple environments. A literature review found that rocket exhaust interference with radar wavelengths is very specific to the particular characteristics of the exhaust, especially its composition. In this year we plan to characterize the radar reflectivity of the various hazards on the terrain field, evaluate the radar under various lander descent profiles (simulated using the Aerial Trolley), characterize and evaluate the sensitivity of the results to moisture content in the simulant, and study (through simulation) the interaction of various exhaust gases with radio frequency signals.</p>","benefits":"<p>Hazard Avoidance is one of the greatest technical challenges for autonomous missions to planetary objectives. The problem's importance is well known and validated by the Agency's investment in systems such as ALHAT. The proposed radar system is much less expensive, lower weight, and draws less electric power than the highly capable ALHAT system. For small, low cost missions these are vital considerations. Compared to optical technologies, radar is more robust in the face of dust and possibly to exhaust turbulence, making the technology especially attractive. Therefore, this proposal explicitly aligns with the strategic areas \"Propulsion testbeds\" and \"Robotic capabilities to accomplish or enhance exploration objectives.\" This proposal seeks to improve MSFC's current technical capability to meet current/future NASA mission needs. Our work also contributes to new NASA capability to land payloads and instruments at targets currently unreachable. This proposal compliments the ALHAT effort and is submitted with the endorsement of the ALHAT project. MSFC has created a new and unique asset, ideal for testing lander hazard avoidance technology, the Lunar Terrain Testbed. The 30mx30m field is covered with high fidelity regolith simulant mined from Merriam Crater, AZ, the source for the JSC-1 family of lunar simulants. It reproduces lunar mineralogy, particle shape, reflectivity, glass content and other characteristics to the maximum practical extent. The testbed responds to rocket exhaust in a manner very comparable to what was observed in the Apollo landings. The field cost ~$60,000 for procurement and site preparation, not counting FTE. At this time (October 2014) the aerial trolley is about to enter service. The aerial trolley is a carrier for sensor packages that rides on a zip line from the top of the Saturn V test stand to a point beyond the lunar terrain field. Testing the radar system on the aerial trolley will enable us to \"fly\" representative landing profiles at much lower cost and higher frequency than possible on a flight system like the Mighty Eagle.</p>","releaseStatus":"Released","status":"Completed","destinationType":[],"trlBegin":4,"trlCurrent":6,"trlEnd":6,"favorited":false,"detailedFunding":false,"programContacts":[],"endDateString":"Oct 2015","startDateString":"Nov 2014"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2014-09-30","technologyOutcomePath":"Advanced_To","details":"FY15 CIF \"Radar Hazard Identification for Planetary Landers Stage 2\"","infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Radar Hazard Identification for Planetary Landers D Stage 2)","isIndirect":false,"infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateFullString":"September 2014","technologyOutcomeDateString":"Sep 2014","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced To","technologyOutcomeRationalePretty":""}],"primaryImage":{"file":{"fileExtension":"jpg","fileId":356583,"presignedUpload":false,"fileSizeString":"0 Byte"},"libraryItemId":356041,"description":"Dust Cloud as the mighty Eagle Traverses the Lunar Terrain Testbed at MSFC","projectId":14742,"publishedDateString":"","libraryItemTypePretty":"","entryDateString":"","modifiedDateString":""},"libraryItems":[{"file":{"fileExtension":"jpg","fileId":356583,"fileName":"Mighty Eagle - Rickman","fileSize":244194,"objectId":356041,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"238.5 KB"},"files":[{"fileExtension":"jpg","fileId":356583,"fileName":"Mighty Eagle - Rickman","fileSize":244194,"objectId":356041,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"238.5 KB"}],"libraryItemId":356041,"title":"Figure 1","description":"Dust Cloud as the mighty Eagle Traverses the Lunar Terrain Testbed at MSFC","libraryItemType":"Image","projectId":14742,"isPrimary":true,"internalOnly":false,"publishedDateString":"","libraryItemTypePretty":"Image","entryDateString":"01/22/25 01:10 AM","modifiedDateString":"05/22/23 02:25 PM"}],"states":[{"abbreviation":"AL","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Alabama","stateTerritoryId":18,"isTerritory":false}],"endDateString":"Sep 2014","startDateString":"Oct 2013"}}