NASA NTRS · 20090011278
Variable-Structure Control of a Model Glider Airplane
Abstract
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.
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Waszak, Martin R., Anderson, Mark R.. 2008-07-01. Variable-Structure Control of a Model Glider Airplane. https://ntrs.nasa.gov/citations/20090011278
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