Flight Simulator Column Force Modeling by System Identification-Reference-Cited by-同舟云学术

Flight Simulator Column Force Modeling by System Identification

Published:2023-06-16 Issue: Volume: Page:
ISSN:
Container-title:2023 The 15th International Conference on Computer Modeling and Simulation
language:
Short-container-title:

Author:

Cai Xiangqun¹^ORCID,Lei Xiaoyong¹^ORCID,Dai Shuling¹^ORCID,Li Weiqi²^ORCID

Affiliation:

1. State Key Lab. of Virtual Reality Technology and Systems, Beihang University, China

2. School of Automation Science and Electrical Engineering, Beihang University, China

Publisher

ACM

Link

https://dl.acm.org/doi/pdf/10.1145/3608251.3608290

Reference16 articles.

1. Horizontally opposed pressure loaded computer generated artificial feel control column for a motion base flight simulation system using fused hard & amp; soft computing

2. Different modeling technologies of hydraulic load simulator for thrust vector control actuator

3. Chinese Civil Aviation Regulations PART 6 0 : Qualification and use of Flight Simulation Training Devices . Civil Aviation Administration of China , Beijing , 2006 . Chinese Civil Aviation Regulations PART 60: Qualification and use of Flight Simulation Training Devices. Civil Aviation Administration of China, Beijing, 2006.

4. THOMPSON J G. Aircraft /control system simulation. IEEE Conference on Control Applications, IEEE Piscataway, NJ. USA , 1996: 119-124. THOMPSON J G. Aircraft/control system simulation. IEEE Conference on Control Applications, IEEE Piscataway, NJ. USA, 1996: 119-124.

5. XU X F, FENG Y C. Aircraft flight control system.Beijing: Beihang University Press , 1989 : 210-240. XU X F, FENG Y C. Aircraft flight control system.Beijing: Beihang University Press, 1989: 210-240.