国防科技大学学报
國防科技大學學報
국방과기대학학보
JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY
2015年
3期
148-154
,共7页
丁智坚%蔡洪%杨华波%连丁磊
丁智堅%蔡洪%楊華波%連丁磊
정지견%채홍%양화파%련정뢰
浮球式惯性平台%自标定%自对准%扩展卡尔曼滤波
浮毬式慣性平檯%自標定%自對準%擴展卡爾曼濾波
부구식관성평태%자표정%자대준%확전잡이만려파
floated inertial platform%self-calibration%self-alignment%extended Kalman filter
针对浮球式惯性平台系统的标定与初始对准问题,提出了一种基于姿态角的连续翻滚自标定自对准方法。根据浮球平台工作原理,建立了惯性器件误差模型,推导了浮球平台的姿态动力学方程;设计了平台在重力场连续翻滚的施矩方案;利用分段线性定常系统和输出灵敏度理论分析了系统的可观性。仿真结果表明,该方法可以同时实现平台系统42项误差系数的高精度标定与初始对准,有效地提高了系统的测量精度。
針對浮毬式慣性平檯繫統的標定與初始對準問題,提齣瞭一種基于姿態角的連續翻滾自標定自對準方法。根據浮毬平檯工作原理,建立瞭慣性器件誤差模型,推導瞭浮毬平檯的姿態動力學方程;設計瞭平檯在重力場連續翻滾的施矩方案;利用分段線性定常繫統和輸齣靈敏度理論分析瞭繫統的可觀性。倣真結果錶明,該方法可以同時實現平檯繫統42項誤差繫數的高精度標定與初始對準,有效地提高瞭繫統的測量精度。
침대부구식관성평태계통적표정여초시대준문제,제출료일충기우자태각적련속번곤자표정자대준방법。근거부구평태공작원리,건립료관성기건오차모형,추도료부구평태적자태동역학방정;설계료평태재중력장련속번곤적시구방안;이용분단선성정상계통화수출령민도이론분석료계통적가관성。방진결과표명,해방법가이동시실현평태계통42항오차계수적고정도표정여초시대준,유효지제고료계통적측량정도。
A continuous self-calibration and self-alignment method based on attitude angle was proposed for the calibration and initial alignment of floated inertial platform (FLIP)system.According to the working principles of floated platform,the inertial sensor error models were built and the attitude dynamic model for the FLIP was established;in order to make the platform to be rotated in the gravity plane,the torquing policy was designed;using the theory of piece wise constant system (PWCS)and output sensitivity,the observability of system was analyzed. Finally,the proposed method was verified by simulations.The simulation results show that the proposed method can synchronously calibrate and align 42 error coefficients of the FLIP with high accuracy and significantly improve the measurement precision of the system.