The dynamic model of a high-performance military aircraft is considered. An input-output representation relating the open-loop pitch and heave rate characteristics to elevator movement is derived. Effective closed-loop design techniques are invoked. Simulated response transients are presented.
Aircraft pitch and heave rate control
2000-01-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aircraft pitch and heave rate control
Online Contents | 2000
|Effects of Heave Washout Settings in Aircraft Pitch Disturbance Rejection
British Library Conference Proceedings | 2009
|Effects of Heave Washout Settings in Aircraft Pitch Disturbance Rejection
Online Contents | 2010
|TRACTION CONTROL CONSIDERING WHEEL SLIP, PITCH AND HEAVE
Europäisches Patentamt | 2016
|