Full State Constrained Stochastic Adaptive Integrated Guidance and Control for STT Missiles with Non-Affine Aerodynamic Characteristics

Kang Chen. Full State Constrained Stochastic Adaptive Integrated Guidance and Control for STT Missiles with Non-Affine Aerodynamic Characteristics. Inf. Sci., 529:42-58, 2020. [doi]

@article{Chen20a-3,
  title = {Full State Constrained Stochastic Adaptive Integrated Guidance and Control for STT Missiles with Non-Affine Aerodynamic Characteristics},
  author = {Kang Chen},
  year = {2020},
  doi = {10.1016/j.ins.2020.03.061},
  url = {https://doi.org/10.1016/j.ins.2020.03.061},
  researchr = {https://researchr.org/publication/Chen20a-3},
  cites = {0},
  citedby = {0},
  journal = {Inf. Sci.},
  volume = {529},
  pages = {42-58},
}