The general flight control laws are designed by static designs and dynamic fits. To improve the adaptive capability, the method of control laws design was introduced by using dynamic optimization genetic algorithms. The control parameters were adjusted online in the flight envelope. The dynamic optimization model was built for aircraft longitudinal function. The fitness was set up by applying order track. And then the control parameters were regulated by dynamic optimization genetic algorithms. Finally an example of a longitudinal control augmented stability system of an aircraft is used with a simulation.
Dynamic Optimization Genetic Algorithms for Flight Control Laws Design
Applied Mechanics and Materials ; 278-280 ; 1581-1584
2013-01-11
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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