Nonlinear Attitude Control ofa Generic Aircraft
Determining suitable controllers for the process of evaluating dynamic per-formance of multiple versions of an aircraft’s aerodynamical, geometric and propulsive properties in its conceptual stage is an expensive task.In this report a proposition is made to utilize a generalized feedback lin-earizin...
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| Format: | Others |
| Language: | English |
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KTH, Flygdynamik
2019
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-261696 |