Attitude Control Law Design Based on LQR for a Compound High-speed Helicopter-Reference-Cited by-同舟云学术

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Attitude Control Law Design Based on LQR for a Compound High-speed Helicopter

Published:2024-05-25 Issue: Volume:23 Page:4147-4151
ISSN:
Container-title:2024 36th Chinese Control and Decision Conference (CCDC)
language:
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Author:

Yin Xinfan¹,Ma Hongxu¹,Wei Qing¹,Jiang Pengfei¹,Wang Liangquan²,Nie Bowen³

Affiliation:

1. National University of Defense Technology,College of Intelligence Science and Technology,Changsha,China

2. China Aerodynamics Research and Development Center,Key Laboratory of Rotor Aerodynamics,Mianyang,China

3. China Aerodynamics Research and Development Center,Low Speed Aerodynamics Institute,Mianyang,China

Funder

Research and Development

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10587298/10587321/10587914.pdf?arnumber=10587914

Reference20 articles.

1. Airbus helicopters X3 flight tests: overview of X3 flight test phase and perspectives for the RACER fast rotorcraft airbus demonstrator;Dominique

2. Clean Sky 2 exploring new rotorcraft high speed configurations;Blacha

3. Research on the scheme of a high-speed helicopter;Wang;Flight Dynamics,2005

4. Pogress of compound helicopter technology;Li;Journal of Nanjing University of Aeronautics & Astronautics,2016

5. Current status, development trend and countermeasure for high-speed rotorcraft;Wang;Journal of Nanjing University of Aeronautics & Astronautics,2015

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