In the Terminal Area energy Management, take advantage of the Energy-Range profile to achieve the flight control of Reusable Launch Vehicle and the energy is also controlled.
末端能量管理段是通过能量—航程的剖面对轨迹飞行器实施控制，并对能量加以控制。
The objective of this paper is to design the reentry flight control laws for the Suborbital Reusable Launch Vehicle(SRLV) based on nonlinear dynamic-inversion.
基于非线性动态逆理论，设计了亚轨道可重复使用运载器（SRLV）的再入控制律。
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。
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