Optimal control of a spacecraft with deployable solar arrays using particle swarm optimization algorithm

DOI10.1007/S11431-011-4350-ZzbMath1237.93121OpenAlexW2049627237MaRDI QIDQ412848

Kai Sun, Xin-Sheng Ge

Publication date: 4 May 2012

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-011-4350-z

zbMATH Keywords

optimal controlattitude dynamicsparticle swarm optimizationmultibody spacecraft

Mathematics Subject Classification ID

Approximation methods and heuristics in mathematical programming (90C59) Nonlinear systems in control theory (93C10) Application models in control theory (93C95)

Related Items (1)

Control strategy of optimal deployment for spacecraft solar array system with initial state uncertainty

Cites Work

• Nonlinear dynamics of a satellite with deployable solar panel arrays
• Optimal control of nonholonomic motion planning for a free-falling cat
• Optimal reorientation of underactuated spacecraft using genetic algorithm with wavelet approximation
• Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
• Motion planning of a nonholonomic multibody system using genetic algorithm
• A novel approach to the attitude control of axisymmetric spacecraft
• Optimal motion planning of an underactuated spacecraft using wavelet approximate method
• Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
• Near-optimal nonholonomic motion planning for a system of coupled rigid bodies

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