DocumentCode :
2200217
Title :
Adaptive nonlinear control of spacecraft near sun-earth L2 lagrange point
Author :
Wong, Hong ; Kapila, Vikram
Author_Institution :
Polytechnic University
Volume :
2
fYear :
2003
fDate :
June 4-6, 2003
Firstpage :
1116
Lastpage :
1121
Keywords :
Adaptive control; Aerodynamics; Aircraft manufacture; Eigenvalues and eigenfunctions; Error correction; Jacobian matrices; Lagrangian functions; Programmable control; Space missions; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
ISSN :
0743-1619
Print_ISBN :
0-7803-7896-2
Type :
conf
DOI :
10.1109/ACC.2003.1239737
Filename :
1239737
Link To Document :
https://search.ricest.ac.ir/dl/search/defaultta.aspx?DTC=49&DC=2200217
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