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