TY - GEN
T1 - Non-cooperative rendezvous and interception - A direct parametric control approach
AU - Duan, Guang Ren
N1 - Publisher Copyright:
© 2014 IEEE.
PY - 2015/3/2
Y1 - 2015/3/2
N2 - In this paper, the dynamical model in a matrix second-order nonlinear form is firstly established in the Sight of Line coordinate system for the problems of non-cooperative rendezvous and interception of spacecrafts, which are complete in the sense that no approximation is taken. Then, with the help of a recently proposed general parametric design approach for general fully-actuated second-order nonlinear systems, a direct parametric approach for spacecraft noncooperative rendezvous and interception control via proportional plus derivative feedback is proposed, which gives a complete parametrization of the pair of feedback gains, and allows usage of the established complete model. The approach possesses two important features. Firstly, with the proposed controller parametrization, the spacecraft rendezvous and the interception systems, though highly nonlinear, can be turned into constant linear systems with desire eigenstructure. Secondly, in such a design there are still degrees of freedom which may be further utilized to improve the system performance. Examples are considered to demonstrate the use of the proposed approach.
AB - In this paper, the dynamical model in a matrix second-order nonlinear form is firstly established in the Sight of Line coordinate system for the problems of non-cooperative rendezvous and interception of spacecrafts, which are complete in the sense that no approximation is taken. Then, with the help of a recently proposed general parametric design approach for general fully-actuated second-order nonlinear systems, a direct parametric approach for spacecraft noncooperative rendezvous and interception control via proportional plus derivative feedback is proposed, which gives a complete parametrization of the pair of feedback gains, and allows usage of the established complete model. The approach possesses two important features. Firstly, with the proposed controller parametrization, the spacecraft rendezvous and the interception systems, though highly nonlinear, can be turned into constant linear systems with desire eigenstructure. Secondly, in such a design there are still degrees of freedom which may be further utilized to improve the system performance. Examples are considered to demonstrate the use of the proposed approach.
KW - Direct parametric approach
KW - Fully-actuated second-order systems
KW - Noncooperative rendezvous
KW - Nonlinear systems
KW - Spacecraft interception
UR - https://www.scopus.com/pages/publications/84932164788
U2 - 10.1109/WCICA.2014.7053297
DO - 10.1109/WCICA.2014.7053297
M3 - 会议稿件
AN - SCOPUS:84932164788
T3 - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
SP - 3497
EP - 3504
BT - Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2014 11th World Congress on Intelligent Control and Automation, WCICA 2014
Y2 - 29 June 2014 through 4 July 2014
ER -