A novel channel phase bias estimation method for spaceborne along-track multi-channel HRWS SAR in time-domain

Author(s):  
Yan-Yang Liu ◽  
Zhen-Fang Li ◽  
Zhi-Yong Suo ◽  
Zheng Bao
2020 ◽  
Vol 12 (1) ◽  
pp. 42-50
Author(s):  
Jianhui Zhao ◽  
Kuan Wang ◽  
Ling Wang ◽  
Zhengwei Guo ◽  
Ning Li

2018 ◽  
Vol 67 (4) ◽  
pp. 831-838 ◽  
Author(s):  
Felipe O. Silva ◽  
Elder M. Hemerly ◽  
Waldemar C. Leite Filho ◽  
Helio K. Kuga

Author(s):  
Yuan Tian ◽  
Marc Compere ◽  
Sergey Drakunov

Abstract Localization accuracy is one of the most important parts of Unmanned Vehicle Systems, Automated Vehicles, Robotics and Navigation. The 6-DOF Inertial Measurement Unit (IMU) is a commonly used device for inertial navigation and is composed of a 3-axis accelerometer and 3-axis gyroscope. The body-fixed IMU measurements are combined with initial values to produce a position and orientation estimate in the inertial frame with every new measurement. However, IMU performance is greatly degraded by bias, scale-factor, non-orthogonality, temperature, and noise. This paper develops a sliding mode observer specifically focused on gyroscope bias estimation to improve gyro measurement results. The work presented here improves the performance of tilt sensors equipped in a commercially available smartphones with accelerometers and gyroscopes. The algorithm uses quaternions to avoid the well-known Euler angle singularities also known as gimbal lock. The observed gyro-bias can be used to reconstruct an improved estimation of the real attitude. A sliding-mode observer was constructed, and A* Matrix stability criterion were used to guarantee observer error convergence in finite time. The algorithm was verified using both a simulated IMU model and experimental tests with a custom designed rotational platform. Simulation tests used a predefined gyros-bias to ensure the algorithm-estimated results converged to the correct value. Simulation results show the observer error quickly converges to zero and the gyro-bias estimation converged to the expected values. The results also show that the proposed method is very effective for reconstructing the real attitude using the observed gyro-bias. This study presents a fast, simple gyro-bias estimation method that can help reconstruct the real attitude with a simple formulation that eliminates complicated constraints.


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