A COMPUTER AIDED DESIGN APPROACH TO AIRBUS A300 FLIGHT CONTROL SYSTEM

1983 ◽  
pp. 453-463 ◽  
Author(s):  
S. Batesha ◽  
D. Viault
Keyword(s):  
Control System ◽  
Flight Control ◽  
Computer Aided Design ◽  
Design Approach ◽  
Flight Control System ◽  
Computer Aided ◽  
Aided Design

scholarly journals Modelling the interplay of security, privacy and trust in sociotechnical systems: a computer-aided design approach

2019 ◽  
Vol 19 (2) ◽  
pp. 467-491 ◽  
Author(s):  
Mattia Salnitri ◽  
Konstantinos Angelopoulos ◽  
Michalis Pavlidis ◽  
Vasiliki Diamantopoulou ◽  
Haralambos Mouratidis ◽  
...  
Keyword(s):  
Computer Aided Design ◽  
Sociotechnical Systems ◽  
Design Approach ◽  
Computer Aided ◽  
Aided Design

Computer Aided Design of a Hydrofoil Control System

1985 ◽  
Vol 18 (8) ◽  
pp. 377-380
Author(s):  
R. Whalley ◽  
P.C. Gregory
Keyword(s):  
Control System ◽  
Computer Aided Design ◽  
Computer Aided ◽  
Aided Design

A Linear Quadratic Integral Design Approach for the Automatic Control System of a Launch Vehicle

2015 ◽  
Vol 772 ◽  
pp. 410-417 ◽  
Author(s):  
Adrian Mihail Stoica ◽  
Cristian Emil Constantinescu ◽  
Silvia Nechita
Keyword(s):  
Control System ◽  
Flight Control ◽  
Launch Vehicle ◽  
Design Approach ◽  
Flight Control System ◽  
Linear Quadratic ◽  
Atmospheric Disturbances ◽  
Modeling Uncertainties ◽  
Quadratic Integral ◽  
The Stability

This paper presents a design approach for the automatic flight control system of a launch vehicle using a linear quadratic integral technique together with a fixed gain Kalman filter. Its purpose is to analyse the stability and tracking robustness performances of the control system designed via this approach when atmospheric disturbances, modeling uncertainties and structural flexible modes of the launcher are taken into account.

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