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Development of Altitude Control System for Autonomous Flight Vehicle
- 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.
Pa Pa Winn San
Zaw Min Aung
Chaw Myat Nwe
Zaw Min Naing