DIGITAL FLIGHT CONTROL SYSTEM DESIGN USING OUTPUT FEEDBACK & MODEL FOLLOWING TECHNIQUES | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 38, Volume 2, A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO, April 1987, Page 975-986 PDF (1.86 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.1987.26195 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| Wahid M. Kassim | ||||
| Col.Dr., Associte Prof., Department of Elect.Equip. & Armament of Aircraft Military Technical College. | ||||
| Abstract | ||||
| Recent advances in control technology provide the means for designing multimode control laws which achieve improved weapon delivery capability and reduced pilot workload. The control objectives for these advanced modes include the ability to command a chosen variable without experiencing significant motion in other, specified varables. Direct tilt Control (Dlr.) is characterized by flight path command without change in angle of attack. Two design methods are used to generate a direct lift control law for an advanced aircraft, fast-samplingerror-actuated digital controllers method and model following technique, (2) Simulation illustrates that fast-sampling error-actuated digital controllers offer several advantages over model following technique. | ||||
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