并应用这两种方法针对视线坐标系的两空间飞行器在目标机动下的追逃进行了理论推导和实验仿真。
Theory analysis and experimental simulations of pursuit-evasion problem with maneuvering target in sight coordinate system are performed using the two methods.
仿真计算结果表明，采用脉冲控制模式，本文提出的安全轨迹制导策略能够实现小卫星临近作业的安全机动飞行。
The results of the simulation indicate that the safety trajectory guidance strategy can achieve safety maneuver flying of the small satellite proximity operation when using thrust control method.
计算仿真表明，该控制器能够较好地发挥飞机的操纵潜力，可使飞机在获得较好的过失速机动能力的同时具有较为满意的飞行品质。
The simulation results have been shown that this controller can take full advantage of aircraft control potential and improve the post stall maneuverability with satisfactory fl...
计算仿真表明，该控制器能够较好地发挥飞机的操纵潜力，可使飞机在获得较好的过失速机动能力的同时具有较为满意的飞行品质。
The simulation results have been shown that this controller can take full advantage of aircraft control potential and improve the post stall maneuverability wi…
计算仿真表明，该控制器能够较好地发挥飞机的操纵潜力，可使飞机在获得较好的过失速机动能力的同时具有较为满意的飞行品质。
The simulation results have been shown that this controller can take full advantage of aircraft control potential and improve the post stall maneuverabil…
以UH 60A直升机在高速飞行条件下的急拉杆机动飞行为例进行仿真计算，并与飞行试验数据进行对比验证。
As an example, a pull-up maneuver of helicopter UH-60A under high speed flight condition is simulated. The correlation of the results with the flight test data is provided.
通过建立动基座对准速度匹配的系统模型，对影响传递对准的一些重要因素如杆臂效应、挠曲振动等进行了分析，按照既定的载机机动方案采集飞行数据进行离线仿真。
By establishing the system model of moving-base alignment velocity match, the factors that influenced the transfer alignment were analyzed, such as lever arm effect, flexible vibrations, etc.
通过建立动基座对准速度匹配的系统模型，对影响传递对准的一些重要因素如杆臂效应、挠曲振动等进行了分析，按照既定的载机机动方案采集飞行数据进行离线仿真。
By establishing the system model of moving-base alignment velocity match, the factors that influenced the transfer alignment were analyzed, such as lever arm effect, flexible vibrations, etc.
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