Partial Integrated Guidance and Control with Impact Angle Constraints
Author:
Affiliation:
1. Department of Mechanics and Aerospace Engineering, College of Engineering, Peking University, 100871 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G000141
Reference38 articles.
1. A Nonlinear Suboptimal Guidance Law with 3D Impact Angle Constraints for Ground Targets
2. Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories
3. Biased PNG law for impact with angular constraint
4. A guidance law with finite time convergence accounting for autopilot lag
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