Optimal control of a satellite-robot system using direct collocation with non-linear programming

V. L. Coverstone-Carroll; N. M. Wilkey

doi:10.1016/0094-5765(95)00096-I

Optimal control of a satellite-robot system using direct collocation with non-linear programming

V. L. Coverstone-Carroll, N. M. Wilkey

Aerospace Engineering

Research output: Contribution to journal › Article › peer-review

Abstract

The non-holonomic behavior of a satellite-robot system is used to develop the system's equations of motion. The resulting non-linear differential equations are transformed into a non-linear programming problem using direct collocation. The link rates of the robot are minimized along optimal reorientations. Optimal solutions to several maneuvers are obtained and the results are interpreted to gain an understanding of the satellite-robot dynamics.

Original language	English (US)
Pages (from-to)	149-162
Number of pages	14
Journal	Acta Astronautica
Volume	36
Issue number	3
DOIs	https://doi.org/10.1016/0094-5765(95)00096-I
State	Published - Aug 1995

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Aerospace Engineering

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10.1016/0094-5765(95)00096-I

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abstract = "The non-holonomic behavior of a satellite-robot system is used to develop the system's equations of motion. The resulting non-linear differential equations are transformed into a non-linear programming problem using direct collocation. The link rates of the robot are minimized along optimal reorientations. Optimal solutions to several maneuvers are obtained and the results are interpreted to gain an understanding of the satellite-robot dynamics.",

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Optimal control of a satellite-robot system using direct collocation with non-linear programming

Abstract

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