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feijicontrol
- 飞行控制系统方案。整个系统由传感器组、飞控计算机、任务管理计算机、舵机、表决电路等主要部件和电源、外总线、通信设备、地面站等辅助设备组成。无人机、起落架、发动机、任务设备、燃油系统、环控系统等是被监控对象。其中，关键传感器采用相似或者非相似三余度；飞控计算机采用“主备备”式三余度飞控机算机；舵机采用二余度电动舵机；表决逻辑由高可靠性单余度数字逻辑电路和双路开关实现。-Flight Control System program. The entire system is composed of s
SIRB
- In this paper it is studied the dynamics of the robotic bird. The system performances are analyzed in terms of time response and robustness. It is study the relation between the angle of attack and the velocity of the bird, the tail influence, the gl
BiologicalRobot
- This paper presents the development of computational simulation and a robotic prototype based on the dynamics of a robotic bird. The study analyze the wing angle of attack and the velocity of the bird, the tail influence, the gliding flight a
Faeering
- 容错系统中关键技术设计及工程实现Fault-tolerant flight control system to achieve key technical design and engineering-Fault-tolerant flight control system to achieve key technical design and engineering
flying-control-law
- 概述了飞行控制律设计的几种主要方法。通过对比自适应飞行控制律和程序调参飞行控制律,总结 了处于飞行控制器设计领域主导地位的程序调参飞行控制律的主要优点和不足,并就程序调参技术在现代飞控领 域的研究现状及其在某先进飞机中的实际应用进行了介绍。最后,针对现代飞机的飞行特点,展望了程序调参飞 行控制律今后可能的发展方向。 -Summarizes the flight control law design of several major method. By comparing the
Vision-Based-Guidance-and-Flight-Control-in-Probl
- paper Vision Based Guidance and Flight Control in Problems of Aerial Tracking
airship.zip
- 无人飞艇在飞行过程中经常受到上升或下降气流的影响，从而使得飞艇的飞行不 稳定，影响任务的执行。本文的主要研究目标为：以ST-3型飞艇为研究对象，针对气 流的影响，设计控制系统。通过控制飞艇发动机推力矢量，即改变飞艇发动机的方向， 向飞艇既提供水平方向的推力，又提供向下或者向上的分力，从而帮助升降舵克服下 降或者上升气流的作用力，使飞艇容易保持预定的高度，提高飞艇的操控性能。具体 工作主要包括以下几个方面：,During the flight, the unmanned airship