On orbit satellite fuel consumption optimization with Analytic Hierarchy Process method

Xin Wang, Wei Wang, Yerong Zhang, Kexin Sun, Lvping Li
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引用次数: 1

Abstract

Analysis of fuel consumption on orbit satellite is presented. The fuel consumption model is nonlinear based on the orbit thruster and attitude control thrusters' misalignment, and is assumed to have unknown dynamics. The issue regarding as the fuel consumption of orbit optimization can be converted to multi-variable optimization with constraint. A modification of the Analytic Hierarchy Process (AHP) optimization algorithm is introduced, by which the fuel consumption estimation models and judgment matrix are established. Simulation results are presented and the optimization design criterion for AHP is also put forward.
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基于层次分析法的在轨卫星燃料消耗优化
对轨道卫星的燃料消耗进行了分析。考虑轨道推力器和姿态控制推力器对中误差的燃料消耗模型是非线性的,并且假定动力未知。轨道优化中的燃料消耗问题可以转化为带约束的多变量优化问题。介绍了对层次分析法(AHP)优化算法的改进,建立了油耗估计模型和判断矩阵。给出了仿真结果,并提出了层次分析法的优化设计准则。
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