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
IEEE Transactions on Aerospace and Electronic Systems ; AES-12 , 6 ; 767-782
01.11.1976
2031333 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Helicopter motion: equation linearization
Tema Archiv | 1976
|Helicopter control design using feedback linearization techniques
Tema Archiv | 1989
|Helicopter Robust Nonlinear Controller Synthesis Using Approximate Linearization
British Library Conference Proceedings | 1993
|