DocumentCode
3450773
Title
Study on the optimal fuel consumption of the singularity condition for lunar soft landing
Author
Shan, Yongzheng ; Duan, Guangren
Author_Institution
Center for Control Theor. & Guidance Technol., Harbin Inst. of Technol., Harbin
fYear
2007
fDate
15-18 Dec. 2007
Firstpage
930
Lastpage
935
Abstract
To achieve the minimal fuel consumption, the Pontryagin maximum principle is utilized to generate an optimal guidance law for the whole process of the lunar probe´s soft landing which starts off from the perilune. It is shown that the singularity condition for the optimal lunar soft landing process doesn´t influence the fuel consumption.
Keywords
aircraft landing guidance; fuel optimal control; maximum principle; space vehicles; Pontryagin maximum principle; lunar soft landing; minimal fuel consumption; optimal fuel consumption; optimal guidance law; singularity condition; Biomimetics; Control theory; Fuels; Gravity; Land surface; Moon; Navigation; Probes; Robot kinematics; Space technology; lunar soft landing; minimal fuel control; singularity condition;
fLanguage
English
Publisher
ieee
Conference_Titel
Robotics and Biomimetics, 2007. ROBIO 2007. IEEE International Conference on
Conference_Location
Sanya
Print_ISBN
978-1-4244-1761-2
Electronic_ISBN
978-1-4244-1758-2
Type
conf
DOI
10.1109/ROBIO.2007.4522288
Filename
4522288
Link To Document