A variable-structure control system designed to enable a fuselage-heavy airplane to recover from spin has been demonstrated in a hand-launched, instrumented model glider airplane. Variable-structure control is a high-speed switching feedback control technique that has been developed for control of nonlinear dynamic systems.
Variable-Structure Control of a Model Glider Airplane
01.07.2008
Sonstige
Keine Angabe
Englisch
Variable Structure Control of a Hand-Launched Glider
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