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Differential geometric guidance command with finite time convergence using extended state observer

  • Mechanical Engineering, Control Science and Information Engineering
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Abstract

For improving the performance of differential geometric guidance command (DGGC), a new formation of this guidance law is proposed, which can guarantee the finite time convergence (FTC) of the line of sight (LOS) rate to zero or its neighborhood against maneuvering targets in three-dimensional (3D) space. The extended state observer (ESO) is employed to estimate the target acceleration, which makes the new DGGC more applicable to practical interception scenarios. Finally, the effectiveness of this newly proposed guidance command is demonstrated by the numerical simulation results.

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Authors and Affiliations

  1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, 410073, China

    Yi-wei Ma  (麻毅威) & Wei-hua Zhang  (张为华)

  2. Unit 61541 of PLA, Beijing, 100094, China

    Yi-wei Ma  (麻毅威)

Authors
  1. Yi-wei Ma  (麻毅威)
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  2. Wei-hua Zhang  (张为华)
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Correspondence to Yi-wei Ma  (麻毅威).

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Ma, Yw., Zhang, Wh. Differential geometric guidance command with finite time convergence using extended state observer. J. Cent. South Univ. 23, 859–868 (2016). https://doi.org/10.1007/s11771-016-3133-x

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  • DOI: https://doi.org/10.1007/s11771-016-3133-x

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