Application of the Improved Incremental Nonlinear Dynamic Inversion in Fixed-Wing UAV Flight Tests-Reference-Cited by-同舟云学术

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Application of the Improved Incremental Nonlinear Dynamic Inversion in Fixed-Wing UAV Flight Tests

Published:2022-11 Issue:6 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Zhenchang¹,Zhang Yufei²^ORCID,Liang JianJian³,Chen Haixin⁴

Affiliation:

1. Postdoctoral Fellow, School of Aerospace Engineering, Tsinghua Univ., Beijing 100084, People’s Republic of China.

2. Associate Professor, School of Aerospace Engineering, Tsinghua Univ., Beijing 100084, People’s Republic of China. ORCID:

3. Ph.D. Student, School of Automation, Beijing Institute of Technology, Beijing 100081, People’s Republic of China.

4. Professor, School of Aerospace Engineering, Tsinghua Univ., Beijing 100084, People’s Republic of China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001495

Reference32 articles.

1. Bauer P. and J. Bokor. 2012. “Tuning and improvements in a waypoint and trajectory tracking algorithm.” In Proc. AIAA Guidance Navigation and Control Conf. 1–19. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-4604.

2. Bhardwaj P. V. S. Akkinapalli J. Zhang S. Saboo and F. Holzapfel. 2019. “Adaptive augmentation of incremental nonlinear dynamic inversion controller for an extended F-16 model.” In Proc. AIAA Scitech 2019 Forum 1–21. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1923.

3. Cakiroglu C. E. Van Kampen and Q. Chu. 2018. “Robust incremental nonlinear dynamic inversion control using angular accelerometer feedback.” In Proc. AIAA Guidance Navigation and Control Conf. 1–16. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2018-1128.

4. Robust Flight Control Design Using Sensor-Based Backstepping Control for Unmanned Aerial Vehicles

5. Extended observer based on adaptive second order sliding mode control for a fixed wing UAV

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