Guidance law modeling based on the ideal line-of-sight with constraint of the terminal flight angle and acceleration

@article{Hao2014GuidanceLM,
  title={Guidance law modeling based on the ideal line-of-sight with constraint of the terminal flight angle and acceleration},
  author={Li Hao and She Haoping},
  journal={The 26th Chinese Control and Decision Conference (2014 CCDC)},
  year={2014},
  pages={1041-1046}
}
  • Li Hao, She Haoping
  • Published 2014 in
    The 26th Chinese Control and Decision Conference…
In the process of pursuing the target, we not only expect the least miss distance, but also a better attitude when the missiles impact the target. The better attitude can effect the power of missiles, and what's more, it can avoid the unnecessary disturbance. For instance, a missile always fails to lock the target owing to the too complicated background while attacking a low-attitude target. The strong surficial background and ground clutter will disturb the seeker's ability to intercept and… CONTINUE READING

From This Paper

Topics from this paper.

Citations

Publications citing this paper.

Path following based on line-of-sight with nonlinear adaptive compensation of side-slip angle

2017 29th Chinese Control And Decision Conference (CCDC) • 2017
View 1 Excerpt
Highly Influenced

References

Publications referenced by this paper.
Showing 1-3 of 3 references

Shima.Intercept Angle Missile Guidance under Time-Varying Acceleration Bounds.AIAA Guidance, Navigation, and Control

Ilan Taub, Tal
2012
View 1 Excerpt

Impact Angle Constrained Interception of Stationary Targets

Ashwini Ratnoo, Debasish Ghose
Journal of guidance , control , and dynamics [ J ]

Linear Quadratic Guidance Laws for Imposing a Terminal Intercept Angle

V Shaferman, T. Shima
Journal of guidance , control , and dynamics [ J ]

Similar Papers

Loading similar papers…