基于微型固体推力器阵列的轨道控制点火算法

Ignition algorithm of solid propellant micro-thruster array for orbit control

为了解决基于微型固体推力器阵列轨道控制的推力器组合点火问题,优化了阵列布局,使其适用于轨道控制,得出了推力器坐标位置分布律。在此基础上研究了推力器阵列组合点火算法,建立了相应数学模型,进行了算法验证。仿真结果表明,设计的推力器阵列优化方案能够满足皮纳卫星轨道控制要求,所建数学模型能有效解决点火问题,设计的算法能够实现较快寻址。

To solve the problem of combined ignition of solid propellant micro-thruster array for orbit control,the layout of micro-thruster array was further optimized to enhance its applicability,and the distribution rule of thruster array was obtained.Combined ignition algorithm with thruster array was proposed.The mathematical model was established and the algorithm was verified.The simulation results show that the requirements of micro-satellite orbit control can be satisfied by the optimal design of thruster array.The mathematic model can solve the ignition problem,and ignition thruster can be addressed quickly by the proposed algorithm.