飞行控制律,flight control law
1)flight control law飞行控制律
1.Method based on μ-analysis techniques for the clearance offlight control laws;飞行控制律评估与确认的μ分析方法
2.Study on Flight Control Law Based on Synthesized Nonlinear Control method基于综合非线性控制方法的飞行控制律研究
3.The bifurcation tailoring technique is used as a global and continuous design method for the nonlinearflight control law.研究了非线性飞行控制律的全局连续设计方法——分支裁剪技术。
英文短句/例句
1.Research on Nonlinear Flight Control Law Design of Aircraft with Vectoring Thrust;推力矢量飞机非线性飞行控制律设计研究
2.Study on Flight Control Law Based on Synthesized Nonlinear Control method基于综合非线性控制方法的飞行控制律研究
3.The Reconfiguration of the Self-Repairing Flight Control Law for Fighters Using Neural Networks;基于神经网络的歼击机自修复飞行控制律重构
4.Design and Simulation of Helicopter Flight Control Law Based on Matlab基于Matlab的直升机飞行控制律设计与仿真
5.Exploring Nonlinear Flight Control of Highly Maneuvering Fighter Aircraft非线性结构自适应模型逆飞行控制律设计研究
6.Neural Network PID Design of Flight Control Laws Based on Model-following基于模型跟随的神经网络PID飞行控制律设计
7.Design of Simple Adaptive Sliding-mode Flight Control Laws自适应滑模容错跟踪飞行控制律的设计
8.Super-Maneuver Flight Control Design Using Constrained Adaptive Backstepping约束反推自适应超机动飞行控制律设计
9.Research on Flight Control Law Model Design and Application Method for Conceptual Aircraft Design;飞机总体设计中的飞行控制律模型设计与应用方法研究
10.Reconfigured Control Law Design Based on Mixed Eigenstructure Assignment Approach可重构飞行控制律设计的混合特征结构配置方法研究
11.Alternate Law [flight control law]备用规律〔飞行控制规律〕
12.Flare Law [flight control law]拉平规律〔飞行控制规律〕
13.Direct Law [flight control law]直接控制规律〔飞行控制规律〕
14.Study on Robust Reconfigural Flight Control Law Based on Simple Adaptive Control简单自适应鲁棒飞行重构控制律研究
15.Realization and Simulation of algorithm for full-envelope control law飞行器全包线控制律算法实现及仿真
16.Design of a Sliding Mode Adaptive Control Law for Reconfigurable Flight Control System可重构飞行控制系统的滑模自适应控制律设计
17.Research on Iced Aircraft Flight Dynamics Characteristics and Envelope Protection Control Law结冰飞行动力学特性与包线保护控制律研究
18.Design and Research of Control law for TiltRotor in Transition Flight Phase倾转旋翼机过渡飞行阶段控制律设计研究
相关短句/例句
simplified flight control law简化飞行控制律
1.This paper,based-on the idea of the integration of flight dynamics and control(FD&C) in an aircraft conceptual design process,proposes asimplified flight control law design and evaluation method which is involved in aircraft configuration design.为了在战斗机总体设计中引入飞控系统对性能和品质的协调作用,提出了简化飞行控制律设计和验证的方法,并将其应用到飞机的选型过程中。
3)Robust flight control systems鲁棒飞行控制律
4)clearance of flight control laws飞行控制律评估
1.In this paper a novel improved genetic based analysis method applied toclearance of flight control laws is proposed.传统的飞行控制律评估方法只能对飞行包线内的离散点进行逐点分析,对不确定性参数也只考虑了上下界,分析过程缺乏完整性和系统性。
5)Flight control law design飞行控制律设计
6)flight control law reconstruction飞行控制律重构
延伸阅读
飞机飞行控制飞机飞行控制aircraftflightcontrol稳定和控制飞机的角运动（偏航、俯仰与滚转）以及飞机的重心运动（前进、升降与横移）。分为人工操纵和自动控制两种。人工操纵是驾驶员通过机械操纵系统操纵飞机舵面和油门杆，控制飞机的飞行。自动控制是通过飞行自动控制系统操纵舵面和油门杆，自动控制飞机的飞行。飞机飞行控制采取的是反馈控制原理。飞机和自动控制系统按负反馈的原则组成闭环回路（飞行控制回路），实现对飞机的稳定与控制。在这个闭环回路中被控制量主要有飞机的姿态角、飞行速度、高度和侧向偏离等，控制量是气动控制面的偏角和油门杆的位移。为了确切地描述飞机的运动状态，需要选定适当的坐标系。常用的坐标系是机体坐标系、速度坐标系和地球坐标系。飞行控制系统的功用包括：保持姿态和航向；增稳或控制增稳；控制空速；控制航迹；自动导航；自动着陆；地形跟随、地形回避；自动瞄准；编队飞行；配合自动空中交通管制等。
