考虑具有大运行范围飞控系统的鲁棒控制问题.基于最佳拟合的方法,建立了适合大运行范围的飞行控制系统模型,从而将其转化为一类与摄动参数呈多项式函数关系的不确定性模型.对某模型飞机控制系统,采用文中鲁棒控制方法,对其进行了鲁棒镇定控制设计,仿真结果表明了文中方法的可行性.This paper deals with a class of parametric uncertainty with polynomial form in perturbation parameters.Based on optimal fitting method,a flying control system fitting into wide operation range is established.For some flying control system models,the robust control method is proposed.The simulation demonstrates that the method is pactical
The research work presented in this thesis deals with flight control problems. Based on robust contr...
From the perspective control practitioners, control of dynamics systems subjected to varying paramet...
Unmanned aerial systems have been widely used for variety of civilian applications over the past few...
Les méthodes de synthèse et de validation de lois de pilotage utiliséesdans le milieu industriel aér...
Robust and Adaptive Control shows the reader how to produce consistent and accurate controllers that...
Robustness and reliability are two of the most important properties of all industrial/engineering c...
The robust loop-shaping control methodology is applied in the flight control system design of the C...
Current automatic control system uses linear mathematical models to validate automatic flight contro...
This paper presents the development of a fully non-linear quadrotor aircraft simulator together with...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2004Thesis (M.Sc.) -- ...
A Robust Dynamic Inversion (RDI) flight control law is designed for a large civil aircraft. Classic...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2004Thesis (M.Sc.) -- ...
In this paper an optimal convex controller is designed to control the angle of attack of a FOXTROT a...
AbstractThis paper, describes a LQG and LQR robust controller for the lateral and longitudinal fligh...
The research work presented in this thesis deals with flight control problems. Based on robust contr...
From the perspective control practitioners, control of dynamics systems subjected to varying paramet...
Unmanned aerial systems have been widely used for variety of civilian applications over the past few...
Les méthodes de synthèse et de validation de lois de pilotage utiliséesdans le milieu industriel aér...
Robust and Adaptive Control shows the reader how to produce consistent and accurate controllers that...
Robustness and reliability are two of the most important properties of all industrial/engineering c...
The robust loop-shaping control methodology is applied in the flight control system design of the C...
Current automatic control system uses linear mathematical models to validate automatic flight contro...
This paper presents the development of a fully non-linear quadrotor aircraft simulator together with...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2004Thesis (M.Sc.) -- ...
A Robust Dynamic Inversion (RDI) flight control law is designed for a large civil aircraft. Classic...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2004Thesis (M.Sc.) -- ...
In this paper an optimal convex controller is designed to control the angle of attack of a FOXTROT a...
AbstractThis paper, describes a LQG and LQR robust controller for the lateral and longitudinal fligh...
The research work presented in this thesis deals with flight control problems. Based on robust contr...
From the perspective control practitioners, control of dynamics systems subjected to varying paramet...
Unmanned aerial systems have been widely used for variety of civilian applications over the past few...