TY - GEN
T1 - Online landing site selection considering maneuverability constraint during mars powered descent phase
AU - Ge, Dantong
AU - Gao, Ai
AU - Cui, Pingyuan
N1 - Publisher Copyright:
© 2016, (publisher). All rights reserved.
PY - 2016
Y1 - 2016
N2 - In Mars landing process, smaller hazards like rocks and craters can only be detected when the vehicle is near the surface. The original landing point might be found dangerous and thus the onboard selection of a new landing site and a real-time trajectory generation become the key to the success of the whole mission. In this paper, an autonomous online safe landing site selection considering maneuverability constraint during powered descent phase is proposed. The new landing site is selected based on a novel criterion called Landing Site Selection Index (LSSI). The index includes not only factors like safety of the terrain in view and terminal motion state, but also the maneuverability of the vehicle. A real-time slidingmode guidance is adopted to transfer the vehicle to the updated destination. The online selection and transfer process ensures the safety of the landing mission from multiple aspects. Further Monte Carlo simulations show the effectiveness and robustness of the scheme.
AB - In Mars landing process, smaller hazards like rocks and craters can only be detected when the vehicle is near the surface. The original landing point might be found dangerous and thus the onboard selection of a new landing site and a real-time trajectory generation become the key to the success of the whole mission. In this paper, an autonomous online safe landing site selection considering maneuverability constraint during powered descent phase is proposed. The new landing site is selected based on a novel criterion called Landing Site Selection Index (LSSI). The index includes not only factors like safety of the terrain in view and terminal motion state, but also the maneuverability of the vehicle. A real-time slidingmode guidance is adopted to transfer the vehicle to the updated destination. The online selection and transfer process ensures the safety of the landing mission from multiple aspects. Further Monte Carlo simulations show the effectiveness and robustness of the scheme.
UR - http://www.scopus.com/inward/record.url?scp=85086949293&partnerID=8YFLogxK
U2 - 10.2514/6.2016-1134
DO - 10.2514/6.2016-1134
M3 - Conference contribution
AN - SCOPUS:85086949293
SN - 9781624103896
T3 - 2016 AIAA Guidance, Navigation, and Control Conference
BT - AIAA Guidance, Navigation, and Control Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Guidance, Navigation, and Control Conference, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -