Carrier-based Aircraft Landing Process Safety Simulation Analysis Based on Fuzzy Inference

LI Xiaolei; ZHAO Tingdi

doi:10.7527/S1000-6893.2013.0037

ACTA AERONAUTICAET ASTRONAUTICA SINICA >

2013 , Vol. 34 >Issue 2: 325 - 333

DOI: https://doi.org/10.7527/S1000-6893.2013.0037

Solid Mechanics and Vehicle Conceptual Design

Carrier-based Aircraft Landing Process Safety Simulation Analysis Based on Fuzzy Inference

LI Xiaolei ,
ZHAO Tingdi

Expand

School of Reliability and Systems Engineering, Beihang University, Beijing 100191, China

Received date: 2012-02-24

Revised date: 2012-04-20

Online published: 2012-06-07

Fold

Abstract

Carrier-based aircraft landing is a complex process, its safety largely depending on the control deviation of the pilot which is again influenced by a combination of the state of the physical condition of the pilot, the environment and the equipment (carrier-based aircraft). Taking a certain type of foreign carrier-based aircraft as an example, this paper provides a method of carrier-based aircraft landing process safety modeling and simulation based on fuzzy inference. The uncertainty of pilot control during the process of carrier-based aircraft landing is considered, and this method analyzes the influencing factors of the uncertainty from the point of view of human-machine-environment. A hazard model is presented based on fuzzy inference, on the basis of this model, a safety simulation model of the landing process is proposed. And then the degree of influence of key factors, such as hazard mode, criticality, and hazard occurrence time, etc., is determined from simulation analysis which lays the foundation for safe carrier-based aircraft landing.

Key words： system safety; carrier-based aircraft; landing; safety simulation; fuzzy inference

Cite this article

LI Xiaolei , ZHAO Tingdi . Carrier-based Aircraft Landing Process Safety Simulation Analysis Based on Fuzzy Inference[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013 , 34(2) : 325 -333 . DOI: 10.7527/S1000-6893.2013.0037

References

[1] Shi Q H. Study on control technology for carrier aircraft landing research on carrier landing technology. Harbin: Harbin Engineering University, 2006. (in Chinese) 史青海. 舰载机着舰控制技术研究. 哈尔滨: 哈尔滨工程大学, 2006.
[2] Rudowsky T, Hynes M, Luter M, et al. Review of the carrier approach criteria for carrier-based aircraft phase I: final report. NAWCADPAX/TR-2002-71, 2002.
[3] Yan Z P. Study on the automatic carrier landing system. Shanghai: Fudan University, 2009. (in Chinese) 颜振萍. 舰载机自动着舰控制系统研究. 上海: 复旦大学, 2009.
[4] Li H. Study and design on automatic carrier landing system. Harbin: Harbin Engineering University, 2009. (in Chinese) 李卉. 舰载机自动着舰控制系统研究与设计. 哈尔滨: 哈尔滨工程大学, 2009.
[5] Xu D S, Liu X Y, Wang L X. Influence of changeful wind on landing safety of carrier-based airplane. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(1): 77-81. (in Chinese) 许东松, 刘星宇, 王立新. 变化风场对舰载飞机着舰安全性影响. 北京航空航天大学学报, 2010, 36(1): 77-81.
[6] Shi L. Influence of disturbances on ship-based aircraft’s landing process. Computer Simulation, 2009, 26(12): 46-48, 61.(in Chinese) 施亮. 各扰动对舰载机着舰过程的影响分析. 计算机仿真, 2009, 26(12): 46-48, 61.
[7] National Defense Science and Technology Industry Committee. GJB/Z 99-97 Engineering handbook for system safety. Beijing: Standards Press of China, 1997. 国防科学技术工业委员会. GJB/Z 99-97系统安全工程手册. 北京: 中国标准出版社, 1997.
[8] Chaudemar J C, Bensana E, Seguin C. Model based safety analysis for an unmanned aerial system. Dependable Robots in Human Environments, 2010.
[9] Bretschneider M, Holberg H J, Bode E, et al. Model-based safety analysis of a flap control system. Proceedings of 14th Annual International Symposium, 2004.
[10] Wang Y G, Qu X J. Modeling and simulation of carrier approach and landing. Journal of System Simulation, 2008, 20(24): 6592-6594, 6598.(in Chinese) 王延刚, 屈香菊. 舰载机进舰着舰过程仿真建模. 系统仿真学报, 2008, 20(24): 6592-6594, 6598.
[11] Wang G C, Cheng J, Bao C M, et al. Diagnosis method of aero-engine fault based on fuzzy inference and evidence theory. Journal of Aerospace Power, 2011, 26(9): 2101-2106. (in Chinese) 王古常, 成坚, 鲍传美, 等. 模糊推理和证据理论融合的航空发动机故障诊断. 航空动力学报, 2011, 26(9): 2101-2106.
[12] Du W J. Study of several key problems on fuzzy control system. Xi’an: Xidian University, 1999. (in Chinese) 杜文吉. 模糊控制系统中的若干关键问题研究. 西安: 西安电子科技大学, 1999.
[13] Xing Z Y. Fuzzy modeling and control of complex industrial processes. Beijing: China Academy of Railway Sciences, 2003. (in Chinese) 邢宗义. 复杂工业过程的模糊建模与控制. 北京: 铁道科学研究院, 2003.
[14] Qu X J, Cui H L. Variable strategy pilot model of carrier landing approach. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(11): 993-997. (in Chinese) 屈香菊, 崔海亮. 舰载机进舰任务中的驾驶员变策略控制模型. 北京航空航天大学学报, 2003, 29(11): 993-997.
[15] Li C Z, Xiao Y L, Fang Z P, et al. Military specification: the background and guide for flying quality of piloted airplanes(MIL-F-8785C). Xi’an: Flight Dynamics Journal Office, 1985.(in Chinese) 李成忠, 肖业轮, 方振平, 等. 军用规范-有人驾驶飞机的飞行品质(MIL-F-8785C)的背景资料和使用指南. 西安: 飞行力学杂志社, 1985.
[16] Shi M, Cui H L, Qu X J. Modeling landing signal officer for carrier approach. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(2): 135-138. 石明, 崔海亮, 屈香菊. 舰载飞机进舰降落信号员模型建模.北京航空航天大学学报, 2006, 32(2): 135-138.

Options

Outlines

模态框（Modal）标题

Abstract

Cite this article

References