MODA CONTROL SYSTEM INCORPORATING DERIVATIVE FEEDBACK | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 79, Volume 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, May 1985, Page 1017-1023 PDF (1.16 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.1985.26570 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| M. S. MADY | ||||
| Dept. of Aircraft Electrical Equipment and Armament , Military Technical College, Kobry El-Koba, Cairo, Egypt. | ||||
| Abstract | ||||
| In the present paper we investigate the problem of modal-control using proportional-plus-derivative output-feedback controllers (PD-type). With the derivative part of the feedback, we can get additional information about the system state vector, which are necessary for the solution of the pole-assignment problem. This group of PD-controllers has the advantage of providing additional parameters without increasing the order of the system under control. The additional derivative term of the system output-compared with purely proportional controllers-helps to reduce the overshoots in the system outputs during the transient period, thus it has no effect on the steady-state characteristics of the system, and it also improves the system stability. A sufficient condition for complete pole-assignment of closed-loop system is derived in the form of lemma. A simple and computationally easy design procedure of PD-controllers is developed, and it is applied to the synth-esis of stabilizing systems of a helicopter. | ||||
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