Underwater robot dual-redundancy gesture detecting system
An underwater robot, dual-redundancy technology, applied in the directions of instruments, measuring devices, surveying and navigation, etc., can solve the problems of interference, output heading information error, performance indicators cannot fully meet the navigation needs of operation-level underwater robots, etc. Low-cost, highly complementary effects
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Embodiment 1
[0073] Implementation 1, combined with the attached figure 1 , The attitude detection system of the dual redundant underwater robot of the present invention is composed of a data fusion processor, a MEMS attitude sensor, an electronic compass, a Doppler log, a depth gauge, and an altimeter sensor. The navigation calculation is realized by the microcontroller, and the attitude, speed, depth and height information are output. The output interface 1 of the Doppler log is connected to the input interface 2 of the data fusion processor, the output interface 3 of the electronic compass is connected to the input interface 4 of the data fusion processor, and the output interface 5 of the MEMS attitude sensor is connected to the data fusion processing The input interface 6 of the altimeter, the output interface 7 of the depth gauge is connected to the input interface 8 of the data fusion processor, the output interface 9 of the altimeter is connected to the input interface 10 of the da...
Embodiment 2
[0074] Implementation 2, the operation steps of EKF filtering based on UD decomposition are as follows:
[0075] Step 1: State one-step prediction:
[0076]
[0077] Step 2: UD decomposition:
[0078]
[0079] Step 3: Solve the filter gain matrix:
[0080]
[0081] From formula (3) can get:
[0082]
[0083] Step 4: State Estimation:
[0084]
[0085] Step 5: Estimate the variance matrix:
[0086]
[0087] Through the EKF filtering algorithm based on UD decomposition, the divergence of EKF operation can be avoided, and the stability of the navigation system data fusion algorithm can be effectively improved.
Embodiment 3
[0088] Implementation 3, combined with the attached figure 2 , the steps of the AHRS partial model correction scheme of the integrated navigation system are as follows:
[0089] Step 1: Use the original data of the three-axis magnetometer and the three-axis accelerometer to calculate the heading angle in the geographic coordinate system as the observation information of the navigation system heading;
[0090] Perform tilt compensation on the three-axis raw data of the electronic compass, as shown in formula (7):
[0091]
[0092] The calculation of heading angle is shown in formula (8):
[0093]
[0094] Step 2: Model construction of the attitude and heading part of the integrated navigation system
[0095] Let the angular velocity input value of the Z-axis MEMS gyroscope be The zero bias of the gyro is ε Z , the gyro noise sequence is n r,z . The model of the Z-axis MEMS gyroscope is shown in formula (9):
[0096]
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