Automatic carrier landing system (ACLS) permits high performance carrier-based aircraft to achieve autonomous safe and stable landing, thus its flight control system requires good maneuverability. In this paper, based on system stability theories, test data of F/A-18A fighter aircraft, and the response optimization tools of MATLAB, a novel parameter design method is proposed, and applied to optimizing the parameters of ACLS longitudinal flight control system in a loop by loop and from inside to outside manner. Simulation results show that the system with calibrated parameters has a better performance in responding to the command signal than that of F/A-18A aircraft.
DONG Ran
,
ZHANG Kunpeng
,
WANG Xiaofeng
,
WANG Lipeng
,
LI Jiatong
. Longitudinal maneuverability optimization of flight control in autonomous carrier landing[J]. Science & Technology Review, 2020
, 38(21)
: 144
-149
.
DOI: 10.3981/j.issn.1000-7857.2020.21.018
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