Effect of radar signal error on automatic carrier landing control of carrier-based aircraft

被引：0
|
作者：
Yang B. [1 ]
Liu G. [1 ]
Hong G. [1 ]
机构：
[1] School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing
来源：
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2017年 / 43卷 / 06期
基金：
中国国家自然科学基金;
关键词：
Automatic carrier landing; Carrier landing success rate; Carrier-based aircraft; Radar navigation; Radar signal error;
D O I：
10.13700/j.bh.1001-5965.2016.0475
中图分类号：
学科分类号：
摘要：
The effect of signal error on carrier landing during radar navigation was analyzed based on the automatic carrier landing system (ACLS) of natural carrier-based aircraft and the commissioned main guiding way of radar navigation in carrier landing. According to the components and the functions of the ACLS, the system and the environment of the whole carrier landing simulation were established, and three different kinds of radar error including testing value, delay time and noise were taken into simulation in order to simulate the landing conditions with error. The results were proved correct due to the calculation of carrier landing success rate which became lower as the absolute value of error increased. This method analyzes the effect degree of radar signal error quantitatively, which not only contributes to the study of carrier landing theory, but also possesses guiding significance for engineering design and application. © 2017, Editorial Board of JBUAA. All right reserved.
引用
收藏
页码：1247 / 1253
页数：6
相关论文
共 12 条
  • [1] Xu C.X., Director radar system of carrier-based aircraft landing, Modern Ships and Warships, 4, pp. 34-35, (2003)
  • [2] Dai Z.J., Yan K.W., Tan X., Development and status of foreign carrier radar, Ship Electronic Engineering, 36, 5, pp. 4-7, (2016)
  • [3] Huff R.W., Kessler G.K., Enhanced displays, flight controls and guidance systems for approach and landing: AD/A244 869, (1978)
  • [4] Peng J., Research on the automatic guide and control of carrier-based airplane approach and landing, pp. 45-69, (2001)
  • [5] Li N.J., Measurement accuracy analysis of air defense intelligence radar, Radar Science and Technology, 3, 1, pp. 1-10, (2005)
  • [6] Ni S.X., Electronic and Research of pilot system of carrier-based aircraft landing, Electronic and Electro-optics System, 2, pp. 8-19, (2000)
  • [7] Urnes J.M., Hess R.K., Development of the F/A-18A automatic carrier landing system, Journal of Guidance, Control, and Dynamics, 8, 3, pp. 289-295, (1985)
  • [8] Yang Y.D., Yu J.Y., Direction and Control of Carrier-based Aircraft Landing, pp. 149-152, (2007)
  • [9] Mook D.J., Swanson D.A., Roemer M.J., Et al., Improved noise rejection in automatic carrier landing systems, Journal of Guidance, Control, and Dynamics, 15, 2, pp. 509-519, (1992)
  • [10] Anderson M.R., Inner and outer loop manual control of carrier aircraft landing: AIAA-1996-3877, (1996)
12