Analysis of the inertially symmetric rigid spacecraft time-optimal three-axis reorientation

DOI10.1002/OCA.2243zbMath1357.49141OpenAlexW2292886246MaRDI QIDQ2965295

Jing Li

Publication date: 2 March 2017

Published in: Optimal Control Applications and Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/oca.2243

zbMATH Keywords

control structurecostate optimizationinertially symmetric rigid spacecraftRadau pseudospectral methodtime-optimal three-axis reorientation

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

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Uses Software

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Cites Work

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• A survey of methods available for the numerical optimization of continuous dynamic systems
• Direct trajectory optimization and costate estimation of finite-horizon and infinite-horizon optimal control problems using a Radau pseudospectral method
• Time-optimal reorientation of the rigid spacecraft using a pseudospectral method integrated homotopic approach
• Survey of Numerical Methods for Trajectory Optimization
• Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints
• New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation

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