介绍了自动驾驶仪mp2000的原理及使用方法。并讨论了其在飞行控制系统中的应用与控制作用。
Introduce the principle of autopilot MP2000 and how to use it. Discuss its application in Aircraft-Control-System and its control effect.
这是一个三轴自动飞行控制系统，它由模拟式的控制增稳系统和数字式自动驾驶仪组成。
It is a automatic flight control system for three axes, and consists of analog control augmentation system and digital autopilot.
靶机驾驶员座舱内原来的飞行员座位移除提供额外的空间用于自动化飞行控制系统。
The target drone has the original pilot seat in the cockpit removed to provide additional space for the automated flight control system.
讨论了一种具有飞行与推力综合系统的舰载机自动着舰控制系统的设计方法。
A design method of the automatic control systems with Integrated flight and thrust controls for landing on carrier is discussed in this paper.
气动伺服弹性系统在不确定性摄动下的鲁棒稳定性问题对于带有自动控制系统的弹性飞行器是非常关键的。
Robust stability of the aeroservoelastic systems subjected to the perturbation of uncertainties is very important for elastic flight vehicles with automatic flight control systems.
全部的MH - 60g都装备了自动飞行控制系统，可将飞机保持在特定飞行高度上。
All the MH-60Gs have an automatic flight control system to stabilize the aircraft in typical flight altitudes.
介绍了将DMC - PID串级控制技术应用到无人机无动力飞行时的自动着陆阶段迎角自动控制系统。
DMC-PID bunches control technology in the Angle of attack automatic control system during unpowered flying automatic landing period is introduced.
在飞行控制系统的自动测试中，飞行控制接口信号是必需的。
Interface signal is necessary on ATE for flight control system equipment.
仿真结果表明，设计的自动控制系统能够使滑翔制导炮弹在飞行过程中具有良好的响应特性，方法简单，易于实现。
The simulation results show that the automatic control system can make the guided projectile response perfectly and design method is simple and achieved easily.
余度技术是提高飞行自动控制系统可靠性的有效手段。
The redundancy technique is an effective way to increase reliability.
自动驾驶仪是直升机飞行控制系统的核心，对自动驾驶仪的检测是确保飞行安全的重要环节。
To ensure the flight safety, the flight control system test should be carried out thoroughly. In this paper, the test system is developed for a helicopter autopilot.
本文立足于某飞机飞行控制系统和航空电子系统的现有条件，依据雷达天线的工作方式，提出了三种自动地形防撞的原理方案。
Based on existent conditions of flight control system and avionic system for an aircraft. The paper presents three schemes of automatic terrain anti-collision according to the radar operating way.
控制系统根据传感器参数自动调节气囊的浮升力，达到整机的重力平衡和节能飞行。
The control system automatically regulates the buoyancy force of the gasbag according to parameters of a sensor, so as to achieve the gravity balance and energy-saving flight of the whole aircraft.
控制系统根据传感器参数自动调节气囊的浮升力，达到整机的重力平衡和节能飞行。
The control system automatically regulates the buoyancy force of the gasbag according to parameters of a sensor, so as to achieve the gravity balance and energy-saving flight of the whole aircraft.
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