Adaptive Incremental Nonlinear Dynamic Inversion for Attitude Control of Micro Aerial Vehicles-Reference-Cited by-同舟云学术

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Adaptive Incremental Nonlinear Dynamic Inversion for Attitude Control of Micro Aerial Vehicles

Published:2016-01-01 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Smeur Ewoud J.¹,Chu Q Ping¹,de Croon Guido C.¹

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1390

Reference16 articles.

1. Full quaternion based attitude control for a quadrotor

2. Reentry Flight Controller Design Using Nonlinear Dynamic Inversion

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Model-Based Control Reconfiguration of a Multirotor UAV using Online System Identification by Sparse Regression (SINDYc);AIAA AVIATION 2023 Forum;2023-06-08

2. Fast Loss of Effectiveness Detection on a Quadrotor using Onboard Sensors and a Kalman Estimation Approach;2023 International Conference on Unmanned Aircraft Systems (ICUAS);2023-06-06

3. Attitude Control of a Tilt-rotor Tailsitter Micro Air Vehicle Using Incremental Control;2023 International Conference on Unmanned Aircraft Systems (ICUAS);2023-06-06

4. Adaptive attitude control of UAV based on neural network compensation;Journal of Physics: Conference Series;2023-05-01

5. Accommodating unobservability to control flight attitude with optic flow;Nature;2022-10-19

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