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Indirect Robust Control of Spacecraft via Optimal ...
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由 M Xin 著作2012被引用 83 次 — A new method is proposed for robust control of spacecraft in proximity orbit servicing operations from an optimal control formulation.
Indirect Robust Control of Spacecraft via Optimal ...
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由 M Xin 著作2012被引用 83 次 — A new method is proposed for robust control of spacecraft in proximity orbit servicing operations from an optimal control formulation.
Indirect Robust Control of Spacecraft via Theta-D Optimal ...
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由 M Xin 著作被引用 9 次 — Indirect Robust Control of Spacecraft via Theta-D Optimal Control Solution. Ming Xin and; Hejia Pan. Ming Xin. Mississippi State University.
Indirect Robust Control of Spacecraft via Theta-D Optimal ...
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This paper proposes a new method for robust control of spacecraft from an optimal control formulation. It can be shown in the new formulation that the ...
Indirect Robust Control of Spacecraft via Optimal Control Solution.
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Indirect Robust Control of Spacecraft via Optimal Control Solution. M. Xin, and H. Pan. IEEE Trans. Aerosp. Electron. Syst., 48 (2): 1798-1809 (2012 ).
[PDF] Indirect Robust Control of Spacecraft via Theta-D Optimal ...
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This paper proposes a new method for robust control of spacecraft from an optimal control formulation. It can be shown in the new formulation that the ...
Hejia Pan
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Indirect robust control of spacecraft via optimal control solution. M Xin, H Pan. IEEE Transactions on Aerospace and Electronic Systems 48 (2), 1798-1809, 2012.
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Ming Xin, Hejia Pan
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This paper proposes a new method for robust control of spacecraft from an optimal control formulation. It can be shown in the new formulation that the ...
Indirect robust control of agile missile via Theta-D technique
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2024年10月22日 — Theta-D technique is applied to solve the nonlinear optimal control problem to obtain the final control law. Numerical results show the ...
Rigid spacecraft robust adaptive attitude Stabilization ...
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由 Z Wang 著作2020被引用 14 次 — In this paper, a robust control method is proposed for rigid spacecraft attitude stabilization under inertia matrix uncertainties and external disturbances.
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