Tang Kanghua
National University of Defense Technology
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Publication
Featured researches published by Tang Kanghua.
ieee international conference on electronic measurement & instruments | 2011
Lv Zhaopeng; Tang Kanghua; Wu Meiping
The misalignment angle between DVL and SINS is the key factor in determine the positioning accuracy of the SINS/DVL integrated navigation system. According to the problems appeared in practice, the error model of SINS was analyzed, and the DVL error model based on the misalignment angle online estimation was presented. The kalman filter technology is used to estimate the misalignment angle online in the integrated navigation process. The vessel test results show the variation of the stable estimation value is in the range of 0.1 degree, and the standard deviation is 0.067 degree, which meet the requirement. The navigation results attest the method can improve the positioning accuracy effectively, and prove the conclusion that the misalignment angle is a principal error source in the INS/DVL integrated navigation system.
conference on industrial electronics and applications | 2007
Tang Kanghua; Wu Meiping; Hu Xiaoping
The conventional Kalman filtering algorithm requires the definition of a dynamic and stochastic model, and errors of low cost MEMS-IMU are likely to vary temporally. So the conventional Kalman filter exists limitation in MEMS-IMU/GPS integrated navigation. This paper presented the use of multiple model adaptive estimation(MMAE) where multiple Kalman filters were run in parallel using different dynamic or stochastic models in MEMS-IMU/GPS integrated navigation. And the modified multiple model Kalman filter was used in order to solve the limitation of multiple model adaptive estimation(MMAE). Using static tests, the algorithm designed was validated. The test results show that the modified multiple model Kalman filter can improve performance of MEMS-IMU/GPS integrated navigation system, compared to the conventional Kalman filtering algorithm. And using the designed algorithm, the positioning accuracy is better than 5m and velocity accuracy is better than 0.1m/ s2, and the attitude errors are less than 0.5 degrees on the static condition.
Archive | 2013
Tang Kanghua; He Xiaofeng; Zhang Kaidong; Hu Xiaoping; Li Tao; Jiang Mingming; Guo Yao; Luo Yong
Archive | 2013
Tang Kanghua; Cao Juliang; Pan Xianfei; Wu Wenqi; Hu Xiaoping; Wu Meiping; Jiang Mingming
Archive | 2013
Luo Bing; Wang Ancheng; Jiang Mingming; Hu Xiaoping; Tang Kanghua; He Xiaofeng; Wu Meiping; Zhang Kaidong; Lian Junxiang; Liu Wei
Archive | 2015
Luo Bing; Tang Kanghua; He Xiaofeng; Jiang Mingming; Hu Xiaoping; Wu Meiping; Zhang Kaidong; Lian Junxiang; Liu Wei
Archive | 2014
Tang Kanghua; He Xiaofeng; Pan Xianfei; Hu Xiaoping; Guo Yao; Luo Bing; Luo Yong
Archive | 2013
Li Tao; He Xiaofeng; Zhu Jiancheng; Tang Kanghua; Pan Xianfei; Hu Xiaoping; Luo Bing
Journal of Chinese Inertial Technology | 2011
Tang Kanghua
Archive | 2016
Wu Wenqi; Liu Ke; Tang Kanghua; Li Tao; Wen Kun