High-dynamic vehicle attitude calculation method and system based on multi-sensor inertial navigation system
An inertial navigation system and multi-sensor technology, applied in the field of high-dynamic vehicle attitude calculation methods and systems, can solve the problems of complex vehicle noise, inability to predict and eliminate in advance, errors, etc.
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Embodiment 1
[0079] like figure 1 One aspect shown provides a method for estimating the attitude of a highly dynamic vehicle based on a multi-sensor inertial navigation system, characterized in that it includes the following steps:
[0080] Obtain vehicle-mounted speedometer and accelerometer data, use the vehicle-mounted speedometer to compensate the accelerometer data to obtain the compensated acceleration, obtain the acceleration through motion acceleration suppression processing, and obtain the observed attitude quaternion.
[0081] Obtain the gyroscope data, use the angular velocity value output by the gyroscope, and obtain the state estimation value of the quaternion through the quaternion differential equation.
[0082] By extending Kalman to perform multi-sensor information fusion, the final attitude angle information is output.
[0083] Wherein, the accelerometer data is compensated by using the on-board speedometer to obtain the compensated acceleration including the following f...
Embodiment 2
[0140] Such as figure 2 As shown, a system for applying the aforementioned method is provided, which is characterized in that it includes an accelerometer (1), a speedometer (2), a gyroscope (3), a processor (4) and a filter (5), the The data output end of accelerometer (1), speedometer (2) and gyroscope (3) is connected with the input end of described processor (4), and the data output end of described processor (4) is connected with described filter (5) connected to the input.
[0141] Above, it needs to be explained that: the b system is the carrier coordinate system; the n system is the navigation coordinate system. The conversion relationship between the carrier coordinate system and the navigation coordinate system is as follows: The attitude angle of the carrier is composed of three angles, the rotation around the X axis is the pitch angle, the rotation around the Y axis is the roll angle, and the Z axis is the yaw angle. The three angles are θ, φ, and ψ. Assume t...
Embodiment 3
[0150] In this paper, a 32-bit microprocessor of STM32 with ARM-CortexM3 as the core is used to construct a data acquisition system. The inertial navigation sensor adopts BW-VG500 from BEWIS Sensing Technology Co., Ltd. This is a high-performance MEMS inertial measurement device that integrates a three-axis accelerometer and a three-axis gyroscope. It can accurately measure the parameters of the vehicle. The linear motion speed uses the STM32 module to read the actual vehicle speed of the vehicle OBD system. In the experiment, the raw data measured by the sensor was sampled at a frequency of 100 Hz. The inertial navigation sensor is aligned with the sampling point of the vehicle speed sensor through STM32. Then, send the raw data to the PC using the serial port. Use the extended Kalman filter designed in this application to process the data on the PC, and then use the serial port to send the raw data to the PC. Finally, the results are obtained through curve description. ...
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