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New self-calibration schemes for accelerometers in platform INS

New self-calibration schemes for accelerometers in platform INS
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摘要 To ensure success of precise navigation, it is necessary to carry out in-field calibration for the accelerometers in platform inertial navigation system(PINS) before a mission is launched.Traditional continuous self-calibration methods are not fit for fast calibration of accelerometers because the platform misalignments have to be estimated precisely and the nonlinear coupling terms will affect accuracy. The multi-position methods with a "shape of motion" algorithm also have some existing disadvantages: High precision calibration results cannot be obtained when the accelerometer's output data are used directly and it is difficult to optimize the calibration scheme. Focusing on this field, this paper proposes new fast self-calibration methods for the accelerometers of PINS. A data compression filter is employed to improve the accuracy of parameter estimation because it is impossible to obtain non-biased estimation for accelerometer parameters when using the "shape of motion" algorithm. Besides, continuous calibration schemes are designed and optimized by the genetic algorithm(GA) to improve the observability of parameters. Simulations prove that the proposed methods can estimate the accelerometer parameter more precisely than traditional continuous methods and multi-position methods, and they are more practical to deal with urgent situations than multi-position methods.
出处 《Journal of Systems Science & Complexity》 SCIE EI CSCD 2015年第5期1032-1042,共11页 系统科学与复杂性学报(英文版)
关键词 SELF-CALIBRATION accelerometers data compression genetic algorithm 平台惯导系统 加速度计 校正方案 平台惯性导航系统 校准方法 估计精度 遗传算法 非线性耦合
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  • 1肖正林,钱培贤,徐军辉.三轴平台快速自标定与自对准方法探讨[J].宇航学报,2006,27(2):222-226. 被引量:12
  • 2杨华波,蔡洪,张士峰,李华滨.高精度惯性平台连续自标定自对准技术[J].宇航学报,2006,27(4):600-604. 被引量:29
  • 3Frazier J, Hellings. Application of Extended Kalman Filtering to a Dynamic Laboratory Calibration of an Inertial Navigation System [ R ]. AD-763718 : 32 - 35.
  • 4Kitzersw R A. Design, Development, and Laboratory Test Results of Kalman Filter System-level IMU Calibration Technique [ R]. AD-A046257 : 17 - 26.
  • 5Jiang Y F, Lin Y P. Error estimation of INS ground alignment through observability analysis[J] .IEEE Trans. A.E.S, 1992, 28(1): 92-96.
  • 6陆元九.惯性器件[M].北京:中国宇航出版社.1993.
  • 7Anderson E W.The principles of navlgation[M].Hollis and Carter,1966.
  • 8Robert R.Comparison of inertial navigation system error models in application of IMU transfer alignment[J].AIAA,1997:686-695.
  • 9Bazjw J.In-flight alignment andcalibration of inertial measurement units-Part1:general formulation[J].IEEE Trans.on Aerospace and Electronic Systems,1972,8(4):439-449.
  • 10Nebot E,Durrant-Whyte H.Initial calibration and alignment of an inertial navigation[M].Washington DC,USA:IEEE Computer Society,1997:175-180.

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