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Featured researches published by Tang Kanghua.


ieee international conference on electronic measurement & instruments | 2011

Online estimation of DVL misalignment angle in SINS/DVL integrated navigation system

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

Multiple Model Kalman Filtering for MEMS-IMU/GPS Integrated Navigation

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

MIMU and GNSS information fusion method

Tang Kanghua; He Xiaofeng; Zhang Kaidong; Hu Xiaoping; Li Tao; Jiang Mingming; Guo Yao; Luo Yong


Archive | 2013

Doppler velocity log (DVL) parameter calibration method used for integrated navigation system of underwater inertial navigation system (INS) and DVL

Tang Kanghua; Cao Juliang; Pan Xianfei; Wu Wenqi; Hu Xiaoping; Wu Meiping; Jiang Mingming


Archive | 2013

Acceleration-measuring method by satellite receiver carrier tracking l

Luo Bing; Wang Ancheng; Jiang Mingming; Hu Xiaoping; Tang Kanghua; He Xiaofeng; Wu Meiping; Zhang Kaidong; Lian Junxiang; Liu Wei


Archive | 2015

High dynamic satellite receiver fast capture method based on 2 ms data storage

Luo Bing; Tang Kanghua; He Xiaofeng; Jiang Mingming; Hu Xiaoping; Wu Meiping; Zhang Kaidong; Lian Junxiang; Liu Wei


Archive | 2014

Satellite receiver baseband signal processing method assisted by inertia information

Tang Kanghua; He Xiaofeng; Pan Xianfei; Hu Xiaoping; Guo Yao; Luo Bing; Luo Yong


Archive | 2013

GNSS carrier phase ambiguity solving method based on gyro measurement information constraint

Li Tao; He Xiaofeng; Zhu Jiancheng; Tang Kanghua; Pan Xianfei; Hu Xiaoping; Luo Bing


Journal of Chinese Inertial Technology | 2011

Acceleration aided EKF-PLL and analysis of time delay effect

Tang Kanghua


Archive | 2016

Actual flight data interpolation-based simulated dynamic locus analyzing and generating method

Wu Wenqi; Liu Ke; Tang Kanghua; Li Tao; Wen Kun

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Hu Xiaoping

National University of Defense Technology

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He Xiaofeng

National University of Defense Technology

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Jiang Mingming

National University of Defense Technology

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Lian Junxiang

National University of Defense Technology

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Wu Meiping

National University of Defense Technology

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Luo Bing

National University of Defense Technology

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Pan Xianfei

National University of Defense Technology

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Wu Wenqi

National University of Defense Technology

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Zhang Kaidong

National University of Defense Technology

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Cao Juliang

National University of Defense Technology

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