Add to ORKGA recently developed algorithm for nonlinear system performance analysis has been applied to an F16 aircraft to begin evaluating the suitability of the method for aerospace problems. The algorithm has a potential to be much more efficient than the current methods in performance analysis for aircraft. This paper is the initial step in evaluating this potential
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
Critical performance parameters of a typical combat aircraft are analysed in relation to their depen...
The paper presents a methodology for calculating the gust response of highly flexible aircraft. Two ...
A recently developed algorithm for nonlinear system performance analysis has been applied to an F16 ...
Summary. The current practice to validate flight control laws relies on applying linear analysis too...
this paper is to extend the robustness analysis techniques of linear systems, and in particular the ...
This paper demonstrates how the robust performance analysis framework can be used to determine worst...
A numerical algorithm for computing necessary conditions for performance specifications is developed...
Adaptive control algorithms have the potential to improve performance and reliability of flight cont...
This paper demonstrates how the robust performance analysis framework can be used to determine worst...
A very general and numerically quite robust algorithm has been proposed by Sastry and Gauvrit (1980)...
This article presents a methodology to assess the robust stability and the robust performance of aut...
A numerical algorithm for computing necessary conditions for performance specifications is develop...
This paper introduces an approach to aircraft design and analysis that focuses on the evaluation of ...
The current practice to validate flight control laws relies on applying linear analysis tools to ass...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
Critical performance parameters of a typical combat aircraft are analysed in relation to their depen...
The paper presents a methodology for calculating the gust response of highly flexible aircraft. Two ...
A recently developed algorithm for nonlinear system performance analysis has been applied to an F16 ...
Summary. The current practice to validate flight control laws relies on applying linear analysis too...
this paper is to extend the robustness analysis techniques of linear systems, and in particular the ...
This paper demonstrates how the robust performance analysis framework can be used to determine worst...
A numerical algorithm for computing necessary conditions for performance specifications is developed...
Adaptive control algorithms have the potential to improve performance and reliability of flight cont...
This paper demonstrates how the robust performance analysis framework can be used to determine worst...
A very general and numerically quite robust algorithm has been proposed by Sastry and Gauvrit (1980)...
This article presents a methodology to assess the robust stability and the robust performance of aut...
A numerical algorithm for computing necessary conditions for performance specifications is develop...
This paper introduces an approach to aircraft design and analysis that focuses on the evaluation of ...
The current practice to validate flight control laws relies on applying linear analysis tools to ass...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
Critical performance parameters of a typical combat aircraft are analysed in relation to their depen...
The paper presents a methodology for calculating the gust response of highly flexible aircraft. Two ...