Control system design of flying-wing UAV based on nonlinear methodology
In this paper, A fluid vector rudder flying-wing UAV is employed as the design object, so as to study the nonlinear design method and flight validation. For the maneuvering flight control, this paper presents a control structure. This control structure included the inner loop linearization decouplin...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
KeAi Communications Co., Ltd.
2017-12-01
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| Series: | Defence Technology |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2214914716301398 |