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V. Chobotov (1991)
Spacecraft Attitude Dynamics and Control
C. Fernandes (1991)
A variational approach to optimal nonholonomic motion planning. In: Proceedings of the IEEE International Conference on Robotics and AutomationProceedings of the IEEE International Conference on Robotics and Automation
Roger Johnson (2001)
An Introduction to the BootstrapTeaching Statistics, 23
P. Krishnaprasad (1990)
Geometric Phases, and Optimal Reconfiguration for Multibody Systems1990 American Control Conference
I. Daubechies (1988)
Orthonormal bases of compactly supported waveletsCommunications on Pure and Applied Mathematics, 41
Y.Z. Liu X.S. Ge (1999)
Optimal control of the stretching process of solar arrays on a spacecraft using a genetic algorithmTechnische Mechanik, 19
G. Walsh, Richard Montgomery, Shankar Sastry (1994)
Orientation control of the dynamic satelliteProceedings of 1994 American Control Conference - ACC '94, 1
Panagiotis Tsiotras, M. Corless, J. Longuski (1995)
A novel approach to the attitude control of axisymmetric spacecraftAutom., 31
Ge Xin-sheng, Zhang Qi-zhi, Li Yan-zhu (2000)
Based on wavelet analysis to optimal control of motion planning of space manipulatorApplied Mathematics and Mechanics, 21
C. Fernandes, L. Gurvits, Zexiang Li (1994)
Near-optimal nonholonomic motion planning for a system of coupled rigid bodiesIEEE Trans. Autom. Control., 39
G. Walsh, S. Sastry (1991)
On reorienting linked rigid bodies using internal motions[1991] Proceedings of the 30th IEEE Conference on Decision and Control
M. Reyhanoglu, N. McClamroch (1992)
Planar Reorientation Maneuvers of Space Multibody Systems Using Internal ControlsJournal of Guidance Control and Dynamics, 15
C. Fernandes, L. Gurvits, Zexiang Li (1991)
A variational approach to optimal nonholonomic motion planningProceedings. 1991 IEEE International Conference on Robotics and Automation
M. Zohdy (2018)
Genetic algorithmsRobust Control Systems with Genetic Algorithms
D.E. Goldberg (1989)
Genetic Algorithms in Searching, Optimization and Machine Learning
P. Crouch (1984)
Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body modelsIEEE Transactions on Automatic Control, 29
Ge Xinsheng, Zhang Qi-zhi, Liu Yanzhu (1998)
OPTIMAL CONTROL OF STRETCHING PROCESS OF SOLAR ARRAYS ON SPACECRAFT USING WAVELET EXPANSION METHODActa Mechanica Solida Sinica, 11
C. Fernandes, L. Gurvits, Zexiang Li (1991)
Optimal nonholonomic motion planning
S.S. Sastry G. Walsh (1995)
On reorienting linked rigid bodies using internal motionsIEEE Trans. Rob. Autom., 11
V. Coverstone-Carroll, N. Wilkey (1995)
Optimal control of a satellite-robot system using direct collocation with non-linear programmingActa Astronautica, 36
H. Krishnan, N. McClamroch, M. Reyhanoglu (1993)
Attitude stabilization of a rigid spacecraft using two momentum wheel actuatorsJournal of Guidance Control and Dynamics, 18
Lee Barford, R. Fazzio, David Smith (1992)
An Introduction to Wavelets
G. Walsh (1994)
Orientation control of the dynamic satellite. In: Proceedings of American Control ConferenceProceedings of American Control Conference
P.S. Krishnaprasad (1990)
Geometric phases and optimal reconfiguration for multibody systems. In: Proceedings of American Control ConferenceProceedings of American Control Conference
D. Goldberg (1991)
Real-coded Genetic Algorithms, Virtual Alphabets, and BlockingComplex Syst., 5
Abstract The optimal attitude control of an underactuated spacecraft is investigated in this paper. The flywheels of the spacecraft can somehow only provide control inputs in two independent directions. The dynamic equations are formulated for the spacecraft under a nonholonomic constraint resulting from the constant time-rate of the total angular momentum of the system. The reorientation of such underactuated spacecraft is transformed into an optimal control problem. A genetic algorithm is proposed to derive the control laws of the two flywheels angle velocity inputs. The control laws are approximated by the discrete orthogonal wavelets. The numerical simulations indicate that the genetic algorithm with the wavelet approximation is an effective approach to deal with the optimal reorientation of underactuated spacecraft.
"Acta Mechanica Sinica" – Springer Journals
Published: Aug 1, 2009
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