研究了空天飞行器（ASV）再入跨大气层飞行时的姿态控制问题。
The problems concerning an aerospace vehicle's(ASV) atmospheric reentry flight attitude control system were researched.
研究一种新的空天飞行器基于非线性干扰观测器的轨迹线性化飞行控制方案。
A novel nonlinear disturbance observer-enhanced trajectory linearization control (TLC) structure is applied to an aerospace vehicle (ASV).
因此适于多性能协同优化设计的理论成为空天飞行器概念设计成败的一个关键。
Thus, the theory of synergetic optimization aerospace vehicles is becoming a key problem in designing.
本课题的来源是国家自然科学基金开展的“空天飞行器的若干重大基础问题”的研究计划之一。
This task is just about one of the research "some important and basic problems of the aerospace vehicle" which is carried out by National Natural Science Foundation of China.
该项目实现了以下重要成果：1）完成空天飞行器优化设计理论方法的研究并进行了实验验证；
There are some important results gain from this project: 1) Present a set of synergetic optimization theory and conduct the verification experiments for it;
本文介绍了重大研究计划“空天飞行器的若干重大基础问题”资助项目所取得的一些研究进展及成果应用情况。
In this paper, the progress and its applications of the projects are introduced about the major research plan "Some Key Fundamental Problems of Aerospace Flying Vehicles".
以涡轮和火箭冲压组合动力的工作模式以及飞行器飞行航迹角、迎角等为调参量，构造空天飞行器爬升轨迹优化流程。
The flow chart of optimizing ASP climb track is designed by adjusting some parameters of Euler angle, attack angle, turbine and rocket-ramjet combined cycle work models, etc.
研究了空天飞行器超声速和高超声速飞行条件下六自由度仿真模型，该模型包含了完整的六自由度动力学方程和运动方程。
Six Degrees of Freedom model and simulation of an aerospace vehicle is presented, which includes the whole of kinetic equations and motion equations.
为了获得优化的组合动力空天飞行器爬升轨迹，以一型水平起降空天运载飞行器为依托，针对任务剖面建立典型状态的飞行动力学模型。
To acquire the climb track of Aero-Space Plane, it is established that the flight dynamics model of the Aero-Space Plane which takes off and lands.
为了获得优化的组合动力空天飞行器爬升轨迹，以一型水平起降空天运载飞行器为依托，针对任务剖面建立典型状态的飞行动力学模型。
To acquire the climb track of Aero-Space Plane, it is established that the flight dynamics model of the Aero-Space Plane which takes off and lands.
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