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- W2390904511 abstract "For the nonlinear characteristics of the execution mechanism of the flight control system,in this paper,we select a fighter as the research subject to analyze the effect of nonlinear elements on aircraft longitudinal short-period characteristics.The data of a fighter dynamics is used to study.At first,the Chalk criterion for evaluating short-period FQ is introduced.And then the aircraft system dynamic model containing the nonlinear elements of flight control systems are built.The basic features of different nonlinear element,such as dead zone,backlash and actuator rate limit,are analyzed.At last,through the time-domain simulation the effect of nonlinear elements on flying quality are discussed with the use Chalk criterion.Comparing and analyzing the results,we find that the existence of dead zone,backlash and rate limit can increase the system phase delay and have great adverse effect on the speed of response.The backlash can also make the system damping smaller and the system instable,and finally cause limit loop oscillation." @default.
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- W2390904511 date "2012-01-01" @default.
- W2390904511 modified "2023-09-25" @default.
- W2390904511 title "Effect of nonlinear characteristics of the control system on aircraft longitudinal flying qualities" @default.
- W2390904511 hasPublicationYear "2012" @default.
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