因为这些风载荷是结构上主要的考虑因素，它们很大地影响着飞行控制系统的设计。
Because these wind loads are a major structural consideration, they greatly influence the design of the flight control system.
本文主要进行了无人机自主编队飞行控制系统的设计方法及应用研究。
This dissertation mainly investigated the design and application of autonomous formation flight control system of unmanned aerial vehicles (UAVs).
这是飞行控制系统作用的主要结果。
本文主要研究了闭环控制系统的故障检测和基于故障检测的自适应重构控制在飞行控制系统中的应用。
We mainly research on fault detection of closed-loop control systems and adaptive reconfiguration control based on fault detection and its application on flight control systems.
该飞行控制系统的主要任务是实现实际角度对指令角度的稳定有效跟踪。
The main function of the flight control system is to track the commanded guidance Angle produced by DG guidance curvature command.
通过分析控制律结构、设计方法以及系统调参方法，建立了能够反映现代战斗机飞行控制系统主要功能的控制律设计方法。
By analyzing the structures, designing methods and gain scheduling methods of FCL, the designing techniques of FCL which can indicate the main functions of modern fighters' FCS are established.
然后对高稳定性无人机飞行控制系统进行了系统原理分析和控制律原理分析，提出了设计任务以及应遵循的主要设计原则。
After that a control system of the unmanned helicopter in high stability was analyzed with the system principle and control law, with which the design task and its design rule was proposed.
我们公司提供的这款遥控飞行器控制系统，结构灵活，控制系统可扩大，主要用于地面，海洋表面和高性能车辆等领域。
The Micro Systems, Inc MOdular Networked TArGet control Equipment (MONTAGE) is a flexible, expandable control system for ground, sea surface, and high performance air vehicles.
我们公司提供的这款遥控飞行器控制系统，结构灵活，控制系统可扩大，主要用于地面，海洋表面和高性能车辆等领域。
The Micro Systems, Inc MOdular Networked TArGet control Equipment (MONTAGE) is a flexible, expandable control system for ground, sea surface, and high performance air vehicles.
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