Terminal guidance law based on adding a power integrator approach with autopilot lag

@article{Wang2017TerminalGL,
  title={Terminal guidance law based on adding a power integrator approach with autopilot lag},
  author={Zhao Wang and Qing Cai and Shurong Li},
  journal={2017 29th Chinese Control And Decision Conference (CCDC)},
  year={2017},
  pages={1952-1957}
}
In this paper, a guidance law is proposed based on adding a power integrator approach for intercepting maneuvering targets in the presence of autopilot lag. Considering the missile autopilot as the first-order system, a new robust finite-time terminal guidance law is designed which can handle the targets maneuvering. In the design procedure, assumed that the acceleration of the target is bounded. It is proved that the system state i.e. the line-of-sight (LOS) angular rate and LOS angular… CONTINUE READING

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