机构

• 力学研究所 [2]
• 地质与地球物理研究所 [1]
• 长春光学精密机械与物... [1]

采集方式

• OAI收割 [4]

内容类型

• 期刊论文 [3]
• 会议论文 [1]

发表日期

• 2023 [2]
• 2012 [1]
• 2010 [1]

学科主题

筛选

浏览/检索结果: 共4条，第1-4条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 A Systematic Approach for Inertial Sensor Calibration of Gravity Recovery Satellites and Its Application to Taiji-1 Mission 期刊论文  OAI收割 REMOTE SENSING, 2023, 卷号: 15, 期号: 15, 页码: 3817 作者:  Zhang HY(张昊越);  Xu P(徐鹏);  Ye ZQ(叶宗奇);  Ye, Dong;  Qiang, Lie   |  收藏  |  浏览/下载：33/0  |  提交时间：2023/09/05 satellite gravity  inertial sensor  accelerometer  calibration  gravitational wave detection   Unsupervised Noise Reductions for Gravitational Reference Sensors or Accelerometers Based on the Noise2Noise Method 期刊论文  OAI收割 SENSORS, 2023, 卷号: 23, 期号: 13, 页码: 6030 作者:  Yang ZL(杨智岚);  Zhang HY(张昊越);  Xu P(徐鹏);  Luo ZR(罗子人)   |  收藏  |  浏览/下载：31/0  |  提交时间：2023/09/05 Noise2Noise  deep learning  denoising  accelerometer  inertial sensor   On the design of feed-forward Sigma Delta interface for MEMS based accelerometers 期刊论文  OAI收割 ANALOG INTEGRATED CIRCUITS AND SIGNAL PROCESSING, 2012, 卷号: 72, 期号: 1, 页码: 3-10 作者:  Liang, Wenquan;  Yang, Changchun;  Qiao, Donghai   |  收藏  |  浏览/下载：32/0  |  提交时间：2018/09/26 Analog to digital conversion  Feed forward sigma-delta interface  MEMS  Inertial accelerometer  Compensation filter  Optimal coefficients   Aircraft orientation error correction based on image aided navigation paper (EI CONFERENCE) 会议论文  OAI收割 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010, August 24, 2010 - August 26, 2010, Changchun, China Tao Z.; Yang L.-M. 收藏  |  浏览/下载：19/0  |  提交时间：2013/03/25 In allusion to the character of aircraft orientation error in inertial navigation system increasing with its working time and error accumulation  airborne image aided navigation system is imported in inertial navigation system to combine integrated navigation system. To acquire high orientation accuracy and high matching speed a new algorithm based on multi-scale edge detection and generalized point theory is put forward. At first multi-scale edge detection algorithm is adopted to realize airborne image edge detection  then image matching algorithm is used based on generalized point theory is used to eliminate error accumulation of peg-top excursion and accelerometer error to correction aircraft aircraft pose error to increase navigation accuracy of aircraft. To prove the algorithm is effective and robust  simulative experiment is done. The simulative experiment indicated that aircraft orientation accuracy is better than inertial navigation system  and its orientation error is less than 15 meters after airborne image aided navigation correction. 2010 IEEE.