Sequential Loop Closure Based Adaptive Autopilot Design for a Hypersonic Vehicle
This paper presents a sequential loop closure approach to designing a velocity and altitude tracking au- topilot for a hypersonic vehicle. The control architecture consists of two decoupled control subsystems, one for velocity, the other for altitude. The velocity control subsystem consists of an ad...
| Hoofdauteurs: | , , , , |
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| Gepubliceerd in: |
2016
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| Online toegang: | http://hdl.handle.net/1721.1/101647 |