Application of quadratic optimization to helicopter flight control.
Quadratic optimization applied to helicopter flight control design, assuming constant feedback gains and command step input with zero steady state error
Gray, D. L.↗
Engineering topics
Stevenson, L.
Publications and source records attributed to Stevenson, L..
The use of automatic control theory and a pilot math model in helicopter manual control system synthesis
Using automatic control theory with simple pilot model for synthesizing helicopter landing approach flight director control laws
Collins, D.↗
Two sets of linearized aircraft equations of motion for control system analysis
Developing mathematical model for tandem rotor helicopter for analysis of automatic approach and landing system
Rempfer, P. S.↗