Real-Time Nonlinear Embedded Control for an Autonomous Quadrotor Helicopter
Control system design of aerospace vehicles with actuator saturation is an important practical design problem that many previous approaches to nonlinear autopilot design did not consider. In particular, small unmanned aerial vehicle rotorcraft actuators often have physical limitations such as a rest...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2007-07, Vol.30 (4), p.1049-1061 |
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Sprache: | eng |
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