Three-dimensional Guidance Law with Impact Angle Constraints Considering Autopilot Dynamics
Author:
Affiliation:
1. School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China
2. Ordnance Science and Research Academy of China,Beijing,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10450150/10449968/10451743.pdf?arnumber=10451743
Reference24 articles.
1. Three-Dimensional Nonlinear Guidance Law with Consideration of Autopilot Dynamics;SUN;Journal of Astronautics,2009
2. Impact angle guidance law considering missiles dynamics of autopilot;Xiong;Control and Decision,2015
3. An adaptive variable structure guidance law considering missiles dynamics of autopilot;She;Journal of Astronautics,2003
4. Bank-to-Turn Guidance Law Using Lyapunov Function and Nonzero Effort Miss
5. A guidance law with finite time convergence accounting for autopilot lag
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