A special case of spacecraft optimal attitude control
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Publication:393657
DOI10.1134/S1064230712020086zbMath1278.49023MaRDI QIDQ393657
Publication date: 23 January 2014
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
optimal controlnecessary optimality conditionsPontryagin's maximum principleattitude control.quaternion methodspacecraft reorientation
Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)
Related Items (5)
Optimal control of the reorientation of a spacecraft in the given time with a quadratic performance criterion related to the control and phase variables ⋮ Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn ⋮ Analytical solution of a linear quadratic optimal control problem with control value constraints ⋮ Restricted quadratic optimal control of a spacecraft turning in a fixed time period ⋮ Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality
Cites Work
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