DocumentCode :
624626
Title :
The motion decomposition of power descent section of soft landing on small bodies based on sliding mode and PD control algorithm
Author :
Gan Lingli ; Li Yuanchun
Author_Institution :
Inst. of Electr. & Electron. Eng., Changchun Univ. of Technol., Changchun, China
fYear :
2013
fDate :
9-11 June 2013
Firstpage :
318
Lastpage :
322
Abstract :
In view of the power descent section of soft landing on small bodies, this paper had deduced the system dynamic models of the probe near small bodies under the body-fixed coordinate system. Through the analysis of the model, we decomposed this one phase of the movement into the out-of-plane movement and in plane movement based on the orbital plane. To the out-of-plane movement, a nominal height trajectory had been projected and variable structure control (VSC) with sliding mode had been designed to track the nominal trajectory. To the in plane movement, according to the coupling of movement and the desired final state, PD controllers are designed to eliminate the deviation of position and velocity. Finally, the effectiveness of algorithms were verified by numerical simulation.
Keywords :
PD control; entry, descent and landing (spacecraft); nucleon-nucleon scattering; numerical analysis; trajectory control; variable structure systems; PD control algorithm; PD controller; body fixed coordinate system; motion decomposition; nominal height trajectory; nominal trajectory; numerical simulation; orbital plane; plane movement; power descent section; sliding mode; soft landing; system dynamic model; variable structure control; Acceleration; Aerodynamics; Navigation; Probes; Robustness; Space vehicles; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Information Processing (ICICIP), 2013 Fourth International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4673-6248-1
Type :
conf
DOI :
10.1109/ICICIP.2013.6568090
Filename :
6568090
Link To Document :
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