Transition Controller Design of Tilt-Rotor UAV Based on Incremental Nonlinear Dynamic Inversion
Author:
Affiliation:
1. School of Astronautics, Northwestern Polytechnical University,Xi'an,China
2. Unmanned System Research Institute, Northwestern Polytechnical University,Xi'an,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10311571/10311610/10312014.pdf?arnumber=10312014
Reference18 articles.
1. L1 Adaptive Structure-Based Nonlinear Dynamic Inversion Control for Aircraft with Center of Gravity Variations
2. Adaptive Neural-Network Controller for an Uncertain Rigid Manipulator With Input Saturation and Full-Order State Constraint
3. Application of the Improved Incremental Nonlinear Dynamic Inversion in Fixed-Wing UAV Flight Tests
4. Three phase induction motor torque ripple minimization based on a novel nonlinear dynamic inverse controller;keream;Proceedings of The National Conference for Postgraduate Research,0
5. Adaptive Fractional-Order Sliding Mode Control for Admittance-Based Telerobotic System With Optimized Order and Force Estimation
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