This article presents a methodology to assess the robust stability and the robust performance of automatic flight control systems (AFCS). The mathematical tool used in the proposed methodology is the structured singular value, µ. For comparison purposes, the paper uses a method largely employed in the aircraft industry to measure the quoted AFCS attributes. The issues existing in this methodology are discussed and it is shown that the proposed method presents one elegant path to deal with the mentioned drawbacks. A step by step procedure is provided, incorporating the advantages offered by the approach currently used in the industry and eliminating its weaknesses
To validate the robust stability of the flight control system of hypersonic flight vehicle, which su...
This work deals with finding the appropriate gains for the flight controller to satisfy the specifi...
This study describes the development and application of new analysis techniques using the structured...
Uma metodologia para avaliar a estabilidade e o desem-penho robustos de sistemas automáticos de coma...
tigated the potential of a number of advanced analysis techniques for use in the clearance of flight...
Robustness and reliability are two of the most important properties of all industrial/engineering c...
We have presented mathematical connections among three stability criteria: (1) the Nyquist stability...
[Abstract] Due to the continuously increasing design requirements on modern aircraft the robustness ...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX84782 / BLDSC - British Library Do...
Current automatic control system uses linear mathematical models to validate automatic flight contro...
A recently developed algorithm for nonlinear system performance analysis has been applied to an F16 ...
This paper addresses the problem of verifying adaptive control techniques for enabling safe flight i...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
In This Report, Development Of Computer Aided Stability Robustness Analysis (CASRA) Software, Implem...
A Robust Dynamic Inversion (RDI) flight control law is designed for a large civil aircraft. Classic...
To validate the robust stability of the flight control system of hypersonic flight vehicle, which su...
This work deals with finding the appropriate gains for the flight controller to satisfy the specifi...
This study describes the development and application of new analysis techniques using the structured...
Uma metodologia para avaliar a estabilidade e o desem-penho robustos de sistemas automáticos de coma...
tigated the potential of a number of advanced analysis techniques for use in the clearance of flight...
Robustness and reliability are two of the most important properties of all industrial/engineering c...
We have presented mathematical connections among three stability criteria: (1) the Nyquist stability...
[Abstract] Due to the continuously increasing design requirements on modern aircraft the robustness ...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX84782 / BLDSC - British Library Do...
Current automatic control system uses linear mathematical models to validate automatic flight contro...
A recently developed algorithm for nonlinear system performance analysis has been applied to an F16 ...
This paper addresses the problem of verifying adaptive control techniques for enabling safe flight i...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
In This Report, Development Of Computer Aided Stability Robustness Analysis (CASRA) Software, Implem...
A Robust Dynamic Inversion (RDI) flight control law is designed for a large civil aircraft. Classic...
To validate the robust stability of the flight control system of hypersonic flight vehicle, which su...
This work deals with finding the appropriate gains for the flight controller to satisfy the specifi...
This study describes the development and application of new analysis techniques using the structured...