On Constrained Nonlinear Tracking Control of a Small Fixed-wing UAV

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Summary

Three different approaches based on the state dependent Riccati equation (SDRE), Sontag’s formula, and aggressive selection from a satisficing control set are proposed to design the heading and air speed control commands for a small fixed-wing unmanned air vehicles.

Type
article
Published
2007-04-01
Cited by
39
References
24

Keywords

Control theory (sociology), Heading (navigation), Nonlinear system, Riccati equation, State (computer science)

References

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