细长型双自旋静止卫星测控仿真

本文介绍了在计算机上进行细长型双自旋卫星姿态、轨道和重要遥测参数仿真的原理和方案。该方案考虑了卫星章动运动对姿态的影响，根据实时性和精度的要求，模拟卫星实际测控过程，对各种遥测量进行了仿真。基于该方案的仿真程序通过了星地大回路演练的检验，达到了预期的要求和目的。

Operation Control Simulation for Prolate Dual-Spin Geostationary Satellite

The concept and scheme for the simulation of attitude, orbit and important telemetry parameters of prolate dual-spin geostationary satellite have been given in the paper. In the scheme the effects of nutation motion on attitude was considered and all telemetry information was simulated on requirements for accuracy and real-time processing with microcomputer under actual process Of tracking, telemetry and command of satellite. The simulation program based on the scheme was tested via satellite-ground loop training and an expected results achieved.