NASA NTRS · 19690065290
Application of quadratic optimization to helicopter flight control.
Abstract
Quadratic optimization applied to helicopter flight control design, assuming constant feedback gains and command step input with zero steady state error
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Gray, D. L., Rempfer, P. S., Stevenson, L.. 1969-01-01. Application of quadratic optimization to helicopter flight control.. https://ntrs.nasa.gov/citations/19690065290
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