ESA unclassified ESA/IPC(2010)81 For official use Att ... - emits
ESA unclassified ESA/IPC(2010)81 For official use Att ... - emits ESA unclassified ESA/IPC(2010)81 For official use Att ... - emits
ESA/IPC(2010)81beyond the current European state-of-the-art in Navigation, Guidance and Control technologies. The characteristics, inparticular the GNC performance and autonomy requirements, of a NEO sample return mission require an increase inmaturity of the GNC technologies. The TRL objective, 5-6 by 2011, can only be achieved with a close synergy with theAurora technology programme in particular for the key descent and landing phases.In this respect, several past and on-going GNC activities which are directly relevant to the present proposal are listedbelow. Past technology activities were conducted in preparation of the ROSETTA mission, such as the -Autonomous andAdvanced Navigation Techniques- (AANT) study which investigated and evaluated autonomous GNC/FDIR strategiesand concepts applicable to a wide range of interplanetary missions, while the most recent ones are part of the AURORAprogramme. These technology activities deal in particular with the development of an Engineering Model of a multimission(landing, rendezvous, cruise, mobility) optical camera suitable for NEO missions (TRL: 5-6 by 2011) and theassociated Image Processing (IP) algorithms and optical stimulator for the verification and validation of vision basednavigation systems (ViSOS), and the development of hazard mapping and re-targeting functions (TRL: 4-5 by 2009).Also, in support of several vision-based navigation system activities, the Agency has funded the development of a terrainsimulation tool, namely PANGU for Planet and Asteroid Scene Generation Utility, which is capable of synthesizing theterrain of planets and asteroids realistically. In addition, the tool has been extended to provide radar signal return from asmall body. This asset is fundamental to the validation of the objectives of the proposed activity.References- ESA Contract No. 14320 (CCN2), -Tool for Terminal GNC Design for NEO Impactor Impactor Missions (CLEON)-focusing on the development of a software tool for GNC performance assessment in the terminal phase of a NEOImpactor mission- ESA Contract No. 1946 (CCN1), -Autonomous GNC Design for NEO Rendezvous (CLEON+)- focusing on thedevelopment of a software tool for GNC performance assessment in the terminal phase of an autonomous NEOrendezvous mission- ESA Contract No.17338 (CCN3), -Asteroid and Whole Planet Simulation with PANGU- dealing with asteroid craterand irregular lighting conditions modelling- ESA Contract No. 9558, -Autonomous and Advanced Navigation Techniques (AANT)- focusing on autonomousGNC/FDIR strategies and concepts applicable to a wide range of interplanetary missions- ESA Contract No. 15292, -Autonomous Navigation for Interplanetary Missions (AutoNav)-, focusing on theinterplanetary phases- ESA Contract No. 20528, -Optical Flow Navigation system for Landing-, focusing on the final powered descent phaseand involving 3D landmarks matching- ESA Contract No. 156188, -Navigation for Planetary Approach and Landing (NPAL)-, focusing on the development ofa vision based camera breadboard with features extraction capability- ESA Contract No. 18038 (CCN3), -Hazard Avoidance Consolidation Activities-, focusing on the development of hazardmapping and re-targeting functions- ESA contract No 20848 -Multi-purpose Vision-based navigation sensor architecture definition (VisNaV)- dealing withthe detailed design of a multi-mission optical navigation camera suitable for landing, rendezvous, cruise/fly-by andmobilityDeliverablesSW (prototype)HW EM (synergy with Aurora programme)ApplicationCurrent TRL: 2-4 Target TRL: 5-6TRL 5 by Q4 2011Need/Date:ApplicationMission:S/W Clause:GenericOperational SWConsistency with Harmonisation Roadmap and conclusion:N/AContractDuration:Reference toESTER18T8071Page 60 of 60
ESA/IPC(2010)81Annex II – bDetailed Description of National TechnologyDevelopment ActivitiesDetailed activity descriptions are provided in this annex for those M-Class missionscandidates which are entering the definition phase.
- Page 56 and 57: ESA/IPC(2010)81M-Mission Candidate:
- Page 58 and 59: ESA/IPC(2010)81- Brazing of differe
- Page 60 and 61: ESA/IPC(2010)81Current TRL: 4-5 Tar
- Page 62 and 63: ESA/IPC(2010)81L-Mission Candidate:
- Page 64 and 65: ESA/IPC(2010)81the control system a
- Page 66 and 67: ESA/IPC(2010)81Survey of critical c
- Page 68 and 69: ESA/IPC(2010)81Current TRL: 2 Targe
- Page 70 and 71: ESA/IPC(2010)81Radiation hard memor
- Page 72 and 73: ESA/IPC(2010)81L-Mission Candidate:
- Page 74 and 75: ESA/IPC(2010)81Mission:S/W Clause:N
- Page 76 and 77: ESA/IPC(2010)81- At least 2 campaig
- Page 78 and 79: ESA/IPC(2010)81S/W Clause:N/AConsis
- Page 80 and 81: ESA/IPC(2010)81L-Mission Candidate:
- Page 82 and 83: ESA/IPC(2010)81Consistency with Har
- Page 84 and 85: ESA/IPC(2010)81Charge Management Sy
- Page 86 and 87: ESA/IPC(2010)81N/AOptical Bench Dev
- Page 88 and 89: ESA/IPC(2010)81Future Science Theme
- Page 90 and 91: ESA/IPC(2010)81Near-sun power gener
- Page 92 and 93: ESA/IPC(2010)81Breadboard (one dyna
- Page 94 and 95: ESA/IPC(2010)81Advanced 2K JT coole
- Page 96 and 97: ESA/IPC(2010)81CCD radiation charac
- Page 98 and 99: ESA/IPC(2010)81Consistency with Har
- Page 100 and 101: ESA/IPC(2010)81To determine accurat
- Page 102 and 103: ESA/IPC(2010)81Mission:S/W Clause:N
- Page 104 and 105: ESA/IPC(2010)81provide spectrally r
- Page 108 and 109: ESA/IPC(2010)81M-Mission Candidate:
- Page 110 and 111: ESA/IPC(2010)81M-Mission Candidate:
- Page 112 and 113: ESA/IPC(2010)81DeliverablesKID dete
- Page 114 and 115: ESA/IPC(2010)81Prediction of the pe
- Page 116 and 117: ESA/IPC(2010)81Page left intentiona
- Page 118: ESA/IPC(2010)81Justification for Pr
<strong>ESA</strong>/<strong>IPC</strong>(<strong>2010</strong>)<strong>81</strong>beyond the current European state-of-the-art in Navigation, Guidance and Control technologies. The characteristics, inparticular the GNC performance and autonomy requirements, of a NEO sample return mission require an increase inmaturity of the GNC technologies. The TRL objective, 5-6 by 2011, can only be achieved with a close synergy with theAurora technology programme in particular for the key descent and landing phases.In this respect, several past and on-going GNC activities which are directly relevant to the present proposal are listedbelow. Past technology activities were conducted in preparation of the ROSETTA mission, such as the -Autonomous andAdvanced Navigation Techniques- (AANT) study which investigated and evaluated autonomous GNC/FDIR strategiesand concepts applicable to a wide range of interplanetary missions, while the most recent ones are part of the AURORAprogramme. These technology activities deal in particular with the development of an Engineering Model of a multimission(landing, rendezvous, cruise, mobility) optical camera suitable for NEO missions (TRL: 5-6 by 2011) and theassociated Image Processing (IP) algorithms and optical stimulator for the verification and validation of vision basednavigation systems (ViSOS), and the development of hazard mapping and re-targeting functions (TRL: 4-5 by 2009).Also, in support of several vision-based navigation system activities, the Agency has funded the development of a terrainsimulation tool, namely PANGU for Planet and Asteroid Scene Generation Utility, which is capable of synthesizing theterrain of planets and asteroids realistically. In addition, the tool has been extended to provide radar signal return from asmall body. This asset is fundamental to the validation of the objectives of the proposed activity.References- <strong>ESA</strong> Contract No. 14320 (CCN2), -Tool for Terminal GNC Design for NEO Impactor Impactor Missions (CLEON)-focusing on the development of a software tool for GNC performance assessment in the terminal phase of a NEOImpactor mission- <strong>ESA</strong> Contract No. 1946 (CCN1), -Autonomous GNC Design for NEO Rendezvous (CLEON+)- focusing on thedevelopment of a software tool for GNC performance assessment in the terminal phase of an autonomous NEOrendezvous mission- <strong>ESA</strong> Contract No.17338 (CCN3), -Asteroid and Whole Planet Simulation with PANGU- dealing with asteroid craterand irregular lighting conditions modelling- <strong>ESA</strong> Contract No. 9558, -Autonomous and Advanced Navigation Techniques (AANT)- focusing on autonomousGNC/FDIR strategies and concepts applicable to a wide range of interplanetary missions- <strong>ESA</strong> Contract No. 15292, -Autonomous Navigation for Interplanetary Missions (AutoNav)-, focusing on theinterplanetary phases- <strong>ESA</strong> Contract No. 20528, -Optical Flow Navigation system for Landing-, focusing on the final powered descent phaseand involving 3D landmarks matching- <strong>ESA</strong> Contract No. 156188, -Navigation for Planetary Approach and Landing (NPAL)-, focusing on the development ofa vision based camera breadboard with features extraction capability- <strong>ESA</strong> Contract No. 18038 (CCN3), -Hazard Avoidance Consolidation Activities-, focusing on the development of hazardmapping and re-targeting functions- <strong>ESA</strong> contract No 20848 -Multi-purpose Vision-based navigation sensor architecture definition (VisNaV)- dealing withthe detailed design of a multi-mission optical navigation camera suitable for landing, rendezvous, cruise/fly-by andmobilityDeliverablesSW (prototype)HW EM (synergy with Aurora programme)ApplicationCurrent TRL: 2-4 Target TRL: 5-6TRL 5 by Q4 2011Need/Date:ApplicationMission:S/W Cla<strong>use</strong>:GenericOperational SWConsistency with Harmonisation Roadmap and conclusion:N/AContractDuration:Reference toESTER18T8071Page 60 of 60