| 引用本文: | 赵岩,高社生,丁晓,等.平流层飞艇抗风场干扰约束Unscented卡尔曼滤波算法设计与应用.[J].国防科技大学学报,2017,39(2):64-70.[点击复制] |
| ZHAO Yan,GAO Shesheng,DING Xiao,et al.Design and application on constraints unscented Kalman filter for stratospheric airship with wind field disturbance[J].Journal of National University of Defense Technology,2017,39(2):64-70[点击复制] |
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| 平流层飞艇抗风场干扰约束Unscented卡尔曼滤波算法设计与应用 |
| 赵岩1, 高社生2, 丁晓3, 韦道知1 |
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(1.空军工程大学 防空反导学院， 陕西 西安 710051;2. 西北工业大学 自动化学院， 陕西 西安 710129;3. 中国航发西安动力控制科技有限公司 技术中心， 陕西 西安 710077)
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| 摘要: |
| 为了提高风场干扰环境下飞艇的导航精度，研究飞艇抗风场干扰导航算法。在建立风场干扰条件下飞艇速度误差约束模型的基础上，设计抗风场干扰的约束Unscented卡尔曼滤波算法。确定风场干扰条件下飞艇的速度误差约束量，将该约束与Unscented卡尔曼滤波算法相结合，对速度误差进行估计和补偿，以减小风场对飞艇定位精度的影响；证明该算法的状态估计量不仅是无偏的，而且协方差小于标准Unscented卡尔曼滤波的协方差；将提出的算法应用于捷联惯导/天文/合成孔径雷达组合导航系统中进行仿真验证，并与自适应扩展卡尔曼滤波和抗差自适应Unscented卡尔曼滤波算法进行比较。结果表明：提出的约束Unscented卡尔曼滤波算法的滤波性能明显优于自适应扩展卡尔曼滤波和抗差自适应Unscented卡尔曼滤波算法，能够有效抑制风场对飞艇定位精度的影响，提高飞艇的导航定位精度。 |
| 关键词: 组合导航 平流层飞艇 风场估计 约束Unscented卡尔曼滤波 |
| DOI：10.11887/j.cn.201702009 |
| 投稿日期：2015-09-16 |
| 基金项目:国家自然科学基金资助项目(61174193) |
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| Design and application on constraints unscented Kalman filter for stratospheric airship with wind field disturbance |
| ZHAO Yan1, GAO Shesheng2, DING Xiao3, WEI Daozhi1 |
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(1. Air and Missile Defense College, Air Force Engineering University, Xi′an 710051, China;2. School of Automatics, Northwestern Polytechnical University, Xi′an 710129, China;3. Technology Center, AECC Xi′an Engine Control Technology Co.Ltd., Xi′an 710077, China)
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| Abstract: |
| To improve the navigation accuracy of airship in the disturbance environment of wind field, a navigation algorithm with anti-interference of wind field was studied. Based on building up an error constraints model of the airship velocity in wind field disturbance, a constraints unscented Kalman filter algorithm which resists wind field disturbance was designed. The error constraint vector of airship velocity was determined. To decrease the impact of wind field on positional accuracy of airship, the velocity error was estimated and compensated by the combination of unscented Kalman filter and error constraint vector. The state estimation value of proposed algorithm was proved to be unbiased, and the covariance was less than that of the standard unscented Kalman filter. The proposed algorithm was applied to SINS/CNS/SAR integrated navigation system and conducted simulation, and was compared with the adaptive extended Kalman filter and robust adaptive unscented Kalman filter. The simulation results show that not only the filter performance of the proposed constraints unscented Kalman filter was much better than those of adaptive extended Kalman filtering and robust adaptive unscented Kalman filter, but also the impact of wind filed on positional accuracy of was reduced and the navigation accuracy of airship was improved effectively. |
| Keywords: integrated navigation stratospheric airship wind filed estimation constraints unscented Kalman filter |
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