2026-05-01T22:40:02Z https://meral.edu.mm/oai

oai:meral.edu.mm:recid/2040 2021-12-13T02:08:27Z 1582963390870:1582967549708 user-uy

Development of Altitude Control System for Autonomous Flight Vehicle Pa Pa Winn San Zaw Min Aung Chaw Myat Nwe Zaw Min Naing The purpose of doing this research is to develop and implement altitude control system for holding of aerial vehicle. This paper emphasizes on the longitudinal stability control system. Experimental autonomous flight vehicle developed by Tamkang University is used as the application airframe as it gives coefficients to get the very accurate model of aircraft flight behaviour. An altitude hold control structure is constructed classical designs. The structure contains two control loops. The inner loop is for altitude rate regulation. In this control loop, the combination of altitude rate and pitch angle are used as the feedback signals. The simulation results of the inner loop are used to design the outer altitude control loop. The inner control loop for this research work is considered in this paper. 2010 http://hdl.handle.net/20.500.12678/0000002040 https://meral.edu.mm/records/2040