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Volume 42 Issue 9
Sep.  2016
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Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(9): 1857-1863.
LI Xinsan, WANG Lixin, WANG Mingjian, et al. Cooperative guidance law based on MPSC and CPN guidance method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1857-1863. doi: 10.13700/j.bh.1001-5965.2015.0592(in Chinese)
Citation: LI Xinsan, WANG Lixin, WANG Mingjian, et al. Cooperative guidance law based on MPSC and CPN guidance method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1857-1863. doi: 10.13700/j.bh.1001-5965.2015.0592(in Chinese)
shu

Cooperative guidance law based on MPSC and CPN guidance method

doi: 10.13700/j.bh.1001-5965.2015.0592
  • 1.

    Department of Control Engineering, Rocket Military Engineering University, Xi'an 710025, China

  • 2. Petty Officer Academy, Rocket Military Engineering University, Qingzhou 262500, China

Funds:  National Natural Science Foundation of China (61203354)
  • Received Date: 10 Sep 2015
  • Publish Date: 20 Sep 2016
    Abstract
  • Cooperative guidance of multiple missiles satisfying terminal impact angle constraints is considered. A suboptimal guidance law is presented using the recently proposed model predictive spread control (MPSC) method and cooperative proportional navigation (CPN) guidance law. The basic principle of the MPSC method is given and the MPSC guidance law is designed on the assumption that the control is considered to be a function of quadratic formulation. The MPSC method requires a control history to begin the algorithmic sequence. Guess control history is computed using the CPN technique, subject to constraint on impact time. A stationary target is attacked by two missiles in the simulation. It is observed from the simulation that the impact time error and terminal impact angle error are within the specified convergence tolerance. The terminal impact angle constraint is well satisfied in salvo attack scenario.

     

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