Research Progress of Planetary Landing Trajectory Optimization Techniques

doi:10.3873/j.issn.1000-1328.2021.06.001

Journal of Astronautics ›› 2021, Vol. 42 ›› Issue (6): 677-686.doi: 10.3873/j.issn.1000-1328.2021.06.001

Previous Articles Next Articles

Research Progress of Planetary Landing Trajectory Optimization Techniques

CUI Ping yuan, LONG Jia teng, ZHU Sheng ying, XIU Wen bo

1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China; 2. Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing 100081, China;3. Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China

Received:2020-06-05 Revised:2020-08-31 Online:2021-06-15 Published:2021-07-22

Abstract

Abstract: Focusing on the high landing safety and accuracy requirements in future planetary landing and sample return missions, the landing dynamic environment and constraints of planetary atmospheric entry and powered descent landing are analyzed. Then, research progress of the planetary landing trajectory optimizations is reviewed. Based on the characteristics of planetary landing trajectory optimization, the key techniques are summarized on the transformation of nonlinear dynamics, optimal trajectory rapid solving under complex constraints, and reachability/controllability analysis under uncertainty.

Key words: Planetary landing, Trajectory optimization, Atmospheric entry, Powered descent, Asteroid soft landing

CLC Number:

V412 4

CUI Ping yuan, LONG Jia teng, ZHU Sheng ying, XIU Wen bo. Research Progress of Planetary Landing Trajectory Optimization Techniques[J]. Journal of Astronautics, 2021, 42(6): 677-686.

[1]	XU Hui, CAI Guang bin, ZHANG Sheng xiu. Modified Aerodynamic Coefficient Fitting Models of Hypersonic Gliding Vehicle in Reentry Phase [J]. Journal of Astronautics, 2021, 42(9): 1139-1149.
[2]	ZHAO Ji song, LI Chang, WANG Chen xi, WANG Tao, ZHU Bo ling, YANG Mei. Boost cruise Trajectory Optimization of Air Breathing Hypersonic Vehicles [J]. Journal of Astronautics, 2021, 42(7): 820-829.
[3]	TIAN Bai yi, WANG Da yi, ZHANG Xiang yu, ZHOU Wen yan, ZHU An wen, HUANG Mei li, WANG Ying. Flight Mission Planning for Solar System Boundary Exploration [J]. Journal of Astronautics, 2021, 42(3): 284-294.
[4]	ZHANG Tao, LI Wei min, LI Jiong, WANG Hua ji, LEI Hu min. Trajectory Optimization of Near space Interceptor with the Constraint of Midcourse and Terminal Guidance Handover Window [J]. Journal of Astronautics, 2021, 42(3): 367-377.
[5]	ZHU Sheng ying, GAO Xi zhen, CUI Ping yuan, YAO Wen long. Integrated Optimization of Navigation Features for Planetary Landing [J]. Journal of Astronautics, 2021, 42(2): 192-201.
[6]	ZHAO Ji song, WANG Jiang hua, WANG Bo qiao, ZHANG Jin ming, ZHU Hang biao. Skip Entry Trajectory Optimization of Lunar Return Vehicles [J]. Journal of Astronautics, 2021, 42(2): 211-219.
[7]	TAN Tian le. Optimization of Propellant Consumption Based on Genetic Algorithm for Spacecraft Rendezvous under Model Predictive and Inversive Control [J]. Journal of Astronautics, 2021, 42(12): 1542-1549.
[8]	HUANG Mei yi, LIANG Zi xuan, CUI Ping yuan. Reachable Zone Generation for Irregularly Shaped Asteroid Landing [J]. Journal of Astronautics, 2021, 42(12): 1550-1558.
[9]	LIU Xu, LI Xiang, ZHANG Hou jun, GUO Yu heng, WANG Xiao peng. Robust Reentry Trajectory Optimization under Uncertainties Using Covariance Analysis Describing Function Technique [J]. Journal of Astronautics, 2021, 42(11): 1404-1415.
[10]	HAO Ze ming, ZHANG Ran, WANG Jia wei, LI Hui feng. Real time Atmospheric Trajectory Optimization for Solid Rockets [J]. Journal of Astronautics, 2021, 42(11): 1416-1426.
[11]	TAN Shu jun, HE Xiao, ZHANG Li yong, WU Zhi gang. Online Trajectory Replanning Method Based on Intelligent Decision making for Launch Vehicles under Thrust Drop Failure [J]. Journal of Astronautics, 2021, 42(10): 1228-1236.
[12]	LIU Kai, GUO Jian, ZHOU Wen ya, SHE Zhi yong. Investigation on Ascent Guidance Law for Air Breathing Combined Cycle Hypersonic Vehicle [J]. Journal of Astronautics, 2020, 41(8): 1023-1031.
[13]	YAO De qing, WEI Yi yin, YANG Zhi hong,CUI Nai gang. Progress and Prospect of Research on Guidance and Control Technology of Aerospace Vehicle#br# [J]. Journal of Astronautics, 2020, 41(7): 850-859.
[14]	YU Yue, WANG Hong lun. A Reentry Trajectory Optimization Method for Hypersonic Vehicles [J]. Journal of Astronautics, 2020, 41(7): 926-936.
[15]	CUI Ping yuan, QIN Tong, ZHU Sheng ying. Progress in Autonomous Navigation and Guidance Technology for Mars Powered Descent Landing [J]. Journal of Astronautics, 2020, 41(1): 1-9.

Research Progress of Planetary Landing Trajectory Optimization Techniques

PDF

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments