Characterising Angular Accelerometer Calibration Setup Disturbance Using Box–Jenkins Method
Author:
Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-65283-2_15
Reference15 articles.
1. Bacon BJ, Ostroff AJ (2000) Reconfigurable flight control using nonlinear dynamic inversion with a special accelerometer implementation. In: Proceedings of the AIAA guidance, navigation and control conference and exhibit. American Institute of Aeronautics and Astronautics, Reston
2. Sieberling S, Chu QP, Mulder JA (2010) Robust flight control using incremental nonlinear dynamic inversion and angular acceleration prediction. J Guid Control Dyn 33(6):1732–1742
3. Jatiningrum D, de Visser CC, van Paassen MM, Mulder M (2016) Modelling an angular accelerometer using frequency response measurement. In: Proceedings of the AIAA guidance, navigation and control conference. American Institute of Aeronautics and Astronautics, Reston
4. Lv P, Liu J, Lai J, Zhang L (2014) Decrease in accuracy of a rotational SINS caused by its rotary table’s errors. Int J Adv Robot Syst 11(74). https://doi.org/10.5772/58579
5. Savage PG (2002) Analytical modeling of sensor quantization in strapdown inertial navigation error equations. J Guid Control Dyn 25(5):833–842
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3