launch vehicle flight system

基本解释

Based on the separation point error calculation, the error variation of missile flight is the premise for system analysis and error distribution of launch vehicle.
依据分离点误差推算弹道飞行的误差变化规律，是进行运载器制导控制系统分析与误差分配的前提条件。
Satellite remote sensing and control system should include flight telemetry and control of launch vehicle, operation telemetry and control of satellite, and telemetry and control of payload equipment.
卫星遥感测控系统包括运载火箭飞行测控、卫星运行测控、有效载荷设备测控以及它本身应完成的遥感测量。