On-orbit application method of solid cold air micro-propulsion module

The invention discloses an on-orbit application method of a solid cold air micro-propulsion module, and belongs to the technical field of space propulsion. According to the method, linear average thrust is conventionally adopted to calculate the orbit control time, a thrust output model of a module is determined through an on-orbit calibration model, and accurate time needed by orbit control is calculated through a nonlinear programming optimization method; the method can be widely applied to high-precision orbit maneuver control and on-orbit calibration of the solid cold air micro-propulsion module. 一种固体冷气微推进模块在轨应用方法，属于空间推进技术领域。本发明常规采用线性化平均推力计算轨控时间的问题，通过在轨标定模型，确定模块的推力输出模型，通过非线性规划优化方法计算获得轨控所需要的精确时间；可广泛应用于固体冷气微推进模块高精度轨道机动控制、在轨标定。