2024-03-29T05:42:03Z
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