Method of Hardware-in-the-Loop (HWIL) Simulation for Pose Movement of Vertical Launching Aerocraft With Continuous Rotation in Yaw

Authors

Chengsheng Liu, 1. Unit 92941 of PLA, Huludao 125001, China;;
Zhang Qing, 2. Beijing Electro-Mechanical Engineering Institute, Beijing 100074, China;

Abstract

Abstract: There are defects in the pose movement simulation of vertical launching aerocraft which can circumrotate continuously in yaw with three -axis flight motion simulator. Based on analysis of these defects, a four-axis project which could be applied to the situation of the changing range of vehicle pitch pose and vehicle roll attitude more than ±180° and the changing range of vehicle course pose towards infinite greatness was proposed. The structure of the four-axis flight motion simulator was analyzed and the control model was made. Above all, a four-axis concerted control law was designed with" switching movement mechanism", and a smooth switch measure in the control process of flight motion simulator was designed too, then the result was validated with simulation. A continuous, real-time and high-efficient simulation method for the pose movement of vertical launching aerocraft which could circumrotate continuously in yaw was confirmed.

Recommended Citation

Liu, Chengsheng and Qing, Zhang (2020) "Method of Hardware-in-the-Loop (HWIL) Simulation for Pose Movement of Vertical Launching Aerocraft With Continuous Rotation in Yaw," Journal of System Simulation: Vol. 28: Iss. 6, Article 11.
Available at: https://dc-china-simulation.researchcommons.org/journal/vol28/iss6/11

First Page

1329

Revised Date

2015-06-19

DOI Link

https://doi.org/

Last Page

1336

CLC

V448.22

Recommended Citation

Liu Chengsheng, Zhang Qing. Method of Hardware-in-the-Loop (HWIL) Simulation for Pose Movement of Vertical Launching Aerocraft With Continuous Rotation in Yaw[J]. Journal of System Simulation, 2016, 28(6): 1329-1336.