论文:2013,Vol:31,Issue(4):511-516
引用本文:
谭雁英, 许鳌, 祝小平, 周洲. 小型无人机掠海飞行高度滤波系统优化设计[J]. 西北工业大学
Tan Yanying, Xu Ao, Zhu Xiaoping, Zhou Zhou. Optimizing and Designing Hybrid Altimeter Filtering System for Small Sea-Skimming Unmanned Aerial Vehicle(UAV)[J]. Northwestern polytechnical university

小型无人机掠海飞行高度滤波系统优化设计
谭雁英, 许鳌, 祝小平, 周洲
西北工业大学 无人机特种技术重点实验室, 陕西 西安 710065
摘要:
针对掠海飞行小型无人机高度控制精度要求,设计了以无线电高度表和垂直加速度计为测高设备的三阶组合测高滤波系统。基于对某小型无人机实际飞行数据以及海浪谱的分析,建立了垂直加速度计和无线电高度表误差模型,推导出该组合测高系统输出高度信号的均方误差关于反馈增益的函数,并采用遗传算法优化得到该函数的极小值和系统的最优反馈增益。仿真结果表明,该三阶组合测高滤波系统可有效滤除海浪噪声,且采用遗传算法优化得到的反馈增益,其滤波效果优于传统上采用等根法得到的反馈增益。
关键词:    小型无人机    掠海飞行    组合测高    垂直加速度计    无线电高度表    遗传算法   
Optimizing and Designing Hybrid Altimeter Filtering System for Small Sea-Skimming Unmanned Aerial Vehicle(UAV)
Tan Yanying, Xu Ao, Zhu Xiaoping, Zhou Zhou
Science and Technology on UAV Laboratory, Northwestern Polytechnic University, Xi'an 710065, China
Abstract:
To achieve the altitude control precision of a small sea-skimming UAV, we design a third-order hybrid altimeter filtering system that uses a radio altimeter and a vertical accelerometer.We analyze the flight data of the vertical accelerometer on the small UAV and the sea wave spectra and then establish the error model of the vertical accelerometer and the sea wave noise model of the radio altimeter.We minimize the mean square error of the output altitude signal of the hybrid altimeter filtering system and use the genetic algorithm to optimize its feedback gains. The simulation results, given in Figs.2 through 6, and their analysis show preliminarily that:(1) our third-order hybrid altimeter filtering system can effectively filter sea wave noise;(2) the feedback gains optimized with the ge-netic algorithm has better filtering results than those obtained with the traditional equivalent root method.
Key words:    accelerometers    altitude control    feedback    genetic algorithms    mathematical models    mean square error    optimization    radio altimeters    spectrum analysis    unmanned aerial vehicles(UAV)    hybrid altimeter    small sea-skimming UAV   
收稿日期: 2012-10-18     修回日期:
DOI:
通讯作者:     Email:
作者简介: 谭雁英(1967-),女,西北工业大学研究员、博士,主要从事无人机自主飞行智能管理及导航控制研究。
相关功能
PDF(583KB) Free
打印本文
把本文推荐给朋友
作者相关文章
谭雁英  在本刊中的所有文章
许鳌  在本刊中的所有文章
祝小平  在本刊中的所有文章
周洲  在本刊中的所有文章

参考文献:
[1] Widnall W S, Sinha P K.Optimizing the Gains of the Baro-Inertial Vertical Channel.Journal of Guidance and Control, 1980, 3 (2): 172-178
[2] Ausman J.Stanley.Baro-Inertial Loop for the USAF Standard RLG INU.Navigation, 1991, 38(2): 205-220
[3] 邵 兵, 赵建波, 刘志伟等.基于维纳滤波法的提高无人机测高精度方法研究.宇航计测技, 2011, 31 (15): 66-69 Shao Bing, Zhao Jianbo, Liu Zhiwei, et al.Altitude Measure Precision of UVA Based on Wiener Filter.Journal of Astronautic Metrology and Measurement, 2011, 31 (15): 66-69 (in Chinese)
[4] 张佑忠.三阶阶组合测高环节的设计.飞航导弹, 1997(1): 14-19 Zhang Youzhong.Design of Third-Order Hybrid Altimeter.Aerodynamic M issile Journal, 1997(1): 14-19(in Chinese)
[5] 许景波, 边信黔, 付明玉.随机海浪的数值仿真与频谱分析.计算机工程与应用, 2010, 46(36): 226-299 Xu Jingbo, Bian Xinqian, Fu Mingyu.Simulation and Spectral Analysis of Random Sea Wave.Computer Engineering and Applications, 2010, 46(36): 226-229 (in Chinese)
[6] 秦永元, 俞济祥.直升机海面悬停时精确高度的维纳滤波提取法.航空学报, 1994, 15(11): 1341-1347 Qin Yongyuan, Yu Jixiang.Extracting the Accurate Height of a Helicopter over Sea via Wiener Filter.Acta Aeronautica et Astronautica Sinica, 1994, 15(11): 1341-1347 (in Chinese)
[7] 王壬林.惯性加速度计与气压高度计之随机误差模型的辨识与估计.航空学报, 1985, 6(6): 556-564 Wang Renlin.Identification and Estimation of the Random Error Models for Inertial Accelerometer and Baro-Altimeter.Acta Aeronautica et Astronautica Sinica, 1985, 6(6): 556-564 (in Chinese)