28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-5.4.2

AEROSERVOELASTIC FLIGHT CONTROL DESIGN FOR A MILITARY COMBAT AIRCRAFT WEAPON SYSTEM

W. G. Luber
CASSIDIAN Air Systems retired; TU Munich, Germany

Keywords: aeroservoelasticity, unsteady aerodynamic, digital flight control system, notch filter

The aim of the aeroservoelastic flight control design is to optimize for a control law forward path and feedback structure the control law parameters like gains, phase advance and notch filters which cover all conditions in a full flight envelope for all possible aircraft external store configurations.

view full paper