The general results of Bradshaw and Porter (1), (2) are extended to allow for a computational time-delay of up to one sampling period by a simple modification of the control algorithms. The resulting control algorithms are simple to implement and provide tight non-interacting control. Their efficiency and effectiveness are demonstrated by the presentation of the results of a laboratory microprocessor implementation in which the controllers are required to effect fuselage pitch-pointing and vertical translation manoevres in the case of an analogue computer representation of the YF-16 aircraft. The general results of Bradshaw and Porter (1), (2) have been extended to allow for a computational time delay of up to one sampling period by a simple modification of the control algorithms. The resulting control algorithms are simple to implement and provide tight non-interacting control. Their efficiency and effectiveness have been demonstrated by the presentation of the results of a laboratory microprocessor implementation in which the controllers were required to effect fuselage pitch pointing and vertical translation manoeuvres in the case of an analogue computer representation of the YF-16 aircraft.
Microprocessor implementation of fast-sampling direct digital flight-mode controllers
Einsatz eines Mikroprozessors in einem schnell samplendem, direktem digitalem Flugkontrollsystem
Agard Conf. Proc. ; 3-8
1983
8 Seiten, 2 Bilder, 7 Quellen
Conference paper
English
Genetic Slow-Mode/Fast-Mode Optimisation of Digital Pid Controllers
British Library Conference Proceedings | 1995
|Digital flight control research using microprocessor technology
Tema Archive | 1979
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