Impact-Time-Control Guidance with Generalized Proportional Navigation Based on Nonlinear Formulation
Author:
Affiliation:
1. Agency for Defense Development, Daejeon 305-152, Republic of Korea
2. Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
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.G001681
Reference12 articles.
1. Homing Guidance Law for Cooperative Attack of Multiple Missiles
2. Impact-time-control guidance law for anti-ship missiles
3. Guidance law to control impact time and angle
4. Augmented Polynomial Guidance With Impact Time and Angle Constraints
5. Hybrid Guidance Law for Approach Angle and Time-of-Arrival Control
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