On Aero Control Law Joined Compensatory PID for Glide down to Fixed Low Altitude System and Simulation Researches
2012 ◽
Vol 198-199
◽
pp. 1021-1024
Keyword(s):
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.
2021 ◽
pp. 014233122110251
2010 ◽
Vol 20
(05)
◽
pp. 1519-1525
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2008 ◽
Vol 130
(4)
◽
Keyword(s):
Keyword(s):
1985 ◽
Vol 107
(4)
◽
pp. 308-315
◽
2014 ◽
Vol 602-605
◽
pp. 1387-1390
Keyword(s):
2020 ◽
Keyword(s):