The nonlinear set of equations which represent helicopter motion is linearized about a prescribed nominal state. Once the linearized system is obtained it is validated by comparing the output of the nonlinear system to that of its linearized counterpart. Having obtained a linear model, linear system theory may then be applied in order to investigate the stability and control characteristics of the aircraft.
Helicopter motion: equation linearization
Hubschrauber-Bewegung: Gleichungslinearisierung
IEEE Transactions on Aerospace and Electronic Systems ; AES-12 , 6. ; 767-782
1976
16 Seiten, 5 Quellen
Article (Journal)
English
Helicopter Motion: Equation Linearization
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