提出了一种针对可重复使用运载器的再入制导算法。
A new reentry guidance algorithm for RLV (reusable launching vehicle) is presented.
新一代可重复使用运载器对再入制导提出了更高地要求。
The new generation of Reusable Launch Vehicles (RLVs) demands improvements to the current entry guidance capability.
建立了可重复使用运载器金属热防护系统瞬态热分析的并联一维模型。
A parallel one-dimensional model for transient thermal analysis of the metallic thermal protection system (MTPS) for reusable launch vehicle (RLV) is established.
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。
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.
可重复使用运载器的防热瓦故障会使航天器的局部结构产生热源，并在结构中形成温度场。
The malfunction of thermal protection system on reusable launch vehicle will generate a heat source on the part of vehicle.
基于古典控制理论和BTT倾斜转弯控制技术，设计了可重复使用运载器(RLV)的大气层内姿态稳定控制系统。
Focused on the problem of reusable launch vehicle (RLV) attitude control, an engineering attitude control system based on the classical control theory and BTT technology was designed.
本文对可重复使用运载器的自适应逆姿态控制进行了研究，以航天飞机轨道器为模型，建立了自适应逆姿态控制的数学模型，设计了自适应逆姿态控制方案。
In this paper, adaptive inverse attitude control of RLV (reusable launch vehicle) is studied. The mathematical model of the orbiter is built and adaptive inverse attitude controller is designed.
本文对可重复使用运载器的自适应逆姿态控制进行了研究，以航天飞机轨道器为模型，建立了自适应逆姿态控制的数学模型，设计了自适应逆姿态控制方案。
In this paper, adaptive inverse attitude control of RLV (reusable launch vehicle) is studied. The mathematical model of the orbiter is built and adaptive inverse attitude controller is designed.
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