Attitude Detection for One-Round Conversation

Author(s):  
Zhaohao Zeng ◽  
Ruihua Song ◽  
Pingping Lin ◽  
Tetsuya Sakai
Keyword(s):  
2014 ◽  
Vol 1039 ◽  
pp. 242-250
Author(s):  
Da Wei Tu ◽  
Xu Zhang ◽  
Kai Fei ◽  
Xi Zhang

Vision measurement for non-cooperative targets in space is an essential technique in space counterwork, fragment disposal, satellite on-orbit service, spacecraft rendezvous, because the position and attitude of the target aircraft or the object should be detected first of all in the process. The 2D passive camera loses the depth information and can not measure the position and attitude of non-cooperative target. Several kinds of range imaging methods are alternatives. The traditional triangulation method can provide very high precision range measurement at close range but the nature of the triangulation geometry means that the uncertainty grows when the range increases. Laser radar (LIDAR) based on TOF (time of flight) or phase difference principle is suitable for middle and long range, but it can not fit for short range. A novel structure system is put forward, in which a so-called synchronous scanning triangulation method is adopted combining a LIDAR system. The synchronous scanning triangulation system plays a role at the range from 0.5m to 10m for object’s attitude, and the LIDAR system plays a role at the range from 10m to 200m for object’s position (direction and range).They are merged into one path, and do not influence each other because of using two different wavelengths respectively. This mechanism makes the system more compact and less weight. The system performances, such as the measurement range and precision, are analyzed according to the system parameters. The principle prototype is designed and established, and the experimental results confirm that its performance is promising and can satisfy the requirement for space application.


2020 ◽  
Vol 20 (11) ◽  
pp. 181
Author(s):  
Tian-Zhu Hu ◽  
Yong Zhang ◽  
Xiang-Qun Cui ◽  
Ye-Ping Li ◽  
Xiu-Shan Pan ◽  
...  

2018 ◽  
Vol 13 (2) ◽  
pp. 198-205 ◽  
Author(s):  
Yiping Rong ◽  
Qunjing Wang ◽  
Siliang Lu ◽  
Guoli Li ◽  
Yin Lu ◽  
...  

Author(s):  
Jiachen Yang ◽  
Meng Xi ◽  
Bin Jiang ◽  
Jiabao Man ◽  
Qinggang Meng ◽  
...  

2018 ◽  
Vol 232 ◽  
pp. 04087
Author(s):  
Long Li ◽  
Jiacai Huang

With the problem of attitude measurement accuracy is susceptible to various errors of geomagnetic survey, this paper establishes geomagnetic measurement error ellipsoid model by analysis of on the environment and own errors, uses the maximum likelihood algorithm for solving the static error correction coefficient. The experimental results show that, the maximum of attitude angle errors is less than 5° near blind direction, online combination correction can ensure the accuracy of attitude detection system under different shooting conditions.


2013 ◽  
Vol 336-338 ◽  
pp. 180-184 ◽  
Author(s):  
Li Long ◽  
He Zhang

The trajectory correction capability of the Simple guided munitions is directly affected by measurement accuracy of attitude angle. A gesture detection method based on geomagnetic gyro combination is proposed in this paper in order to detect the projectile flight attitude, The yaw angle of the projectile is solved by using runge-kutta algorithm with angle information of MEMS gyro. Then roll angle and pitch angle of the projectile is solved by magnetic field component of the three-axis magnetic sensor. Finally, the whole attitude detection system is installed in three-axis non-magnetic turntable to have a performance test. Experimental results show that the attitude solution results error is small. Nearby blind area, the roll angle error reduced to 5° and the pitch angle error reduced to 4°. In other locations, the roll angle error reduced to 2° and the pitch angle error reduce to 1°. The measurement accuracy increased nearly tenfold, can satisfy the trajectory correction demand of simple guidance ammunition.


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