In order to improve accuracy of constant altitude fly at low altitude and fly track of glide down to fixed altitude, aeroplane’s control scheme of glide down to fixed low altitude with PID compensatory link were designed. At the same time, the corresponding control laws had been designed. After simple analysis about working principle of the aeroplane’s control system, simulation researches were done to optimize designed control laws, so that achieving expectant requirement. Simulation results show that designed control scheme and control law were accurate and effective.
On Aero Control Law Joined Compensatory PID for Glide down to Fixed Low Altitude System and Simulation Researches
AMMASS, International Applied Mechanics, Mechatronics Automation & System Simulation Meeting, 2012 ; 1021-1024
Applied Mechanics and Materials ; 198-199
2012
4 Seiten
Conference paper
English
Internal altitude technique for hypersonic glide vehicle guidance
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