DocumentCode
1795381
Title
Next-generation Mars EDL GNC: Challenges and solutions
Author
Xiuqiang Jiang ; Yukai Wang ; Shuang Li
Author_Institution
Coll. of Astronaut., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
2558
Lastpage
2563
Abstract
All Mars landers to date continue to rely on the entry, descent and landing (EDL) technologies developed for the Viking missions in the mid-seventies of the last century. Viking-like landers adopt the inertial navigation and unguided entry mode, which lead to the larger landing error ellipse and lower elevation landing site restriction. Next-generation Mars missions requires the capability of pin-point landing (safe landing within tens of meters to 100 m of a pre-selected target site), the current Mars EDL guidance navigation and control (GNC) system cannot meet the requirements. In this paper, main challenges that impact on Mars EDL GNC are analyzed firstly. Then, some potential solutions are proposed to circumvent the challenges. Integrated navigation schemes are presented to improve the navigation accuracy. At the same time, active entry guidance schemes are proposed to improve the guidance performance with the larger parameter uncertainties using robust and adaptive control theory. Fault-tolerant control strategies are given to enhance the reliability, and the autonomous hazard detection and avoidance scheme is also developed to improve the safety of landing.
Keywords
aerospace safety; collision avoidance; entry, descent and landing (spacecraft); fault tolerant control; hazardous areas; planetary rovers; GNC system; Mars landers; Viking missions; Viking-like landers; active entry guidance schemes; adaptive control theory; autonomous hazard detection; avoidance scheme; elevation landing site restriction; entry descent and landing technologies; fault-tolerant control strategies; guidance navigation and control; inertial navigation; integrated navigation schemes; landing error ellipse; landing safety; navigation accuracy; next-generation Mars EDL GNC; next-generation Mars missions; parameter uncertainties; pin-point landing; reliability; robust control theory; safe landing; unguided entry mode; Accuracy; Adaptation models; Mars; Radio navigation; Trajectory; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007569
Filename
7007569
Link To Document