DocumentCode :
1709469
Title :
A dimension-reduction algorithm for spacecraft control allocation based on the optimal thruster combination table
Author :
Wang Min ; Xie Yongchun
Author_Institution :
Beijing Inst. of Control Eng., Beijing, China
fYear :
2013
Firstpage :
2344
Lastpage :
2349
Abstract :
A new dimension-reduction algorithm based on the optimal thruster combination table for solving the spacecraft thrusters´ control allocation problem is proposed. The general design method of this new algorithm is detailed. The 3-dimension algorithm is cited as an example. And the simulation results demonstrate the advantage of this new dimension-reduction algorithm in being a good compromise among control accuracy, fuel consumption, real time computation speed and space for data storage. Its value in engineering is also pointed out.
Keywords :
aerospace engines; aircraft control; control system synthesis; space vehicles; 3-dimension algorithm; control accuracy; data storage space; design method; dimension-reduction algorithm; fuel consumption; optimal thruster combination table; real-time computation speed; spacecraft control allocation; spacecraft thruster control allocation problem; Aerospace electronics; Algorithm design and analysis; Control engineering; Resource management; Space technology; Space vehicles; Three-dimensional displays; Control Allocation; Dimension Reduction; Spacecraft Thruster;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
Type :
conf
Filename :
6639818
Link To Document :
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