基于气浮平台的飞行器性能验证技术研究

doi:10.16182/j.issn1004731x.joss.201810018

系统仿真学报 ›› 2018, Vol. 30 ›› Issue (10): 3739-3746.doi: 10.16182/j.issn1004731x.joss.201810018

基于气浮平台的飞行器性能验证技术研究

张灏龙, 廖馨, 李彬, 韦文书, 裴胤, 惠俊鹏

中国运载火箭技术研究院研发中心,北京 100076

收稿日期:2016-09-11 修回日期:2016-12-22 出版日期:2018-10-10 发布日期:2019-01-04
作者简介:张灏龙(1977),男,山东,博士,研究员,研究方向为系统仿真与效能评估;廖馨(1980),女,湖北,博士,高工,研究方向为飞行器性能仿真;李彬(1982),男,陕西,硕士,工程师,研究方向为飞行器建模。

Research on Performance Validation of Aircraft Based on Air-table

Zhang Haolong, Liao Xin, Li Bin, Wei Wenshu, Pei Yin, Hui Junpeng

R&D Center, China Academy of Launch Vehicle Technology, Beijing 100076, China

Received:2016-09-11 Revised:2016-12-22 Online:2018-10-10 Published:2019-01-04

摘要/Abstract

摘要： 针对飞行器地面性能验证存在的主要技术问题,将气浮试验技术应用于飞行器试验验证领域,设计并实现了基于气浮平台的飞行器性能验证系统,并提出了空间缩比理论,解决了气浮空间与真实空间的映射关系问题,为在地面开展飞行器性能验证提供了一种技术途径。该系统已应用在某飞行器仿真任务中,表明了其有效性和可用性。

关键词: 气浮平台, 飞行器性能验证, 空间缩比, 气浮模拟器

Abstract: Aiming at the main issues in performance validation of aircraft, this paper applied air-bearing test technology into the area of performance validation of aircraft, designed and established performance validation system of aircraft based on air-bearing. A kind of theory of space scale model was proposed and the mapping relation between air-bearing space and real space was solved. This research provided a new technical approach for performance validation of aircraft. This system has been successfully applied to a kind of aircraft simulation. The Effectiveness and accuracy are verified.

Key words: air-table, performance validation of aircraft, space scale, aircraft simulator

中图分类号:

TP139.9

张灏龙, 廖馨, 李彬, 韦文书, 裴胤, 惠俊鹏. 基于气浮平台的飞行器性能验证技术研究[J]. 系统仿真学报, 2018, 30(10): 3739-3746.

Zhang Haolong, Liao Xin, Li Bin, Wei Wenshu, Pei Yin, Hui Junpeng. Research on Performance Validation of Aircraft Based on Air-table[J]. Journal of System Simulation, 2018, 30(10): 3739-3746.

参考文献

[1] Li Bohu, Chai Xudong, Zhu Wenhai, et al.Some focusing points in development of modern modeling and simulation technology[J]. Journal of System Simulation (S1004-731X), 2004, 16(9): 1871-1878 (in Chinese)
李伯虎, 柴旭东, 朱文海, 等. 现代建模与仿真技术发展中的几个焦点[J]. 系统仿真学报(S1004-731X), 2004, 16(9): 1871-1878.
[2] Jana L Schwartz, Mason A Peck, Christopher D.Hall. Historical Review of Air-Bearing Spacecraft Simulators[J]. Journal of Guidance, Control, and Dynamics (S0731-5090), 2003, 26(4): 513-522.
[3] B N Agrawal, R E Ramussen. Air Bearing Based Satellite Attitude Dynamics Simulator for Control Software Research and Development, Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VI. [C]// Proceedings of SPIE Vol.4366 (2001). USA: SPIE, 2001.
[4] Spencer Michael G, Chernesky Vince, Baker Jeffrey, et al.Bifocal Relay Mirror Experiments on the NPS Three Axis Spacecraft Simulator[C]// AIAA, 2002. USA: AIAA, 2002.
[5] Lau Jimmy, Joshi Sanjay S, Agrawal Brij N, et al.Disturbance filtering and identification on the naval postgraduate school three-axis spacecraft simulator[C]// AIAA. USA: AIAA, 2005: 3771-3791.
[6] Jong-Woo Kim, Roberto Cristi, Brij N.Attitude Determination for NPS Three-Axis Spacecraft Simulator[C]// AIAA/AAS Astrodynamics Specialist Conference and Exhibit 16-19 August, 2004, Providence, Rhode Island, USA. USA: AIAA, 2004.
[7] Shi Xin.Design and Analysis of the Attack and Defense Ground Physical Simulation System [D]. Harbin, China: Harbin Institute of Technology, 2012.
[8] Zhao Xiaoxiong.Navigation and Control of Space Control Technology Verification [D]. Harbin, China: Harbin Institute of Technology, 2013.
[9] Xu Jian, Bao Gang, Yang Qinjun, et al. Design and Development of a 5-DOF Air-Bearing Spacecraft Simulator [C]// International Asia Conference on Informatics in Control, Automation and Robotics, 2009, Bangkok, Thailand.
[10] B J Kim, H Lee.Spacecraft Attitude Dynamics Analysis Using Three-Axis Air Bearing[J]. Space Technology (S0892-9270), 1997, 17(1): 45-50.
[11] J Prado, G Bisiachig, L Reyes, et al.Three-axis air-bearing based platform for small satellite attitude determination and control simulation[J]. Journal of Applied Research and Technology (S1665-6423), 2005, 3(3): 222-237.
[12] Ning Dejin.The Design and Implementation of System for Controlling Single-Axis Air Bearing Table [D]. Harbin, China: Harbin Institute of Technology, 2009.

基于气浮平台的飞行器性能验证技术研究

Research on Performance Validation of Aircraft Based on Air-table

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