VTOL UAV Transition Maneuver Using Incremental Nonlinear Dynamic Inversion
The paper seeks to study the control system design of a novel unmanned aerial vehicle (UAV). The UAV is capable of vertical takeoff and landing (VTOL), transition flight and cruising via the technique of direct force control. The incremental nonlinear dynamic inversion (INDI) approach is adopted for...
Main Authors: | Zhenchang Liu, Jie Guo, Mengting Li, Shengjing Tang, Xiao Wang |
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Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2018-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2018/6315856 |
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