Polynomial Shaping of the Look Angle for Impact-Time Control
Author:
Affiliation:
1. Aselsan Inc., 06750 Ankara, Turkey
2. Roketsan Missiles Inc., 06780 Ankara, Turkey
3. Technical University of Munich, 85748 Munich, Germany
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
https://arc.aiaa.org/doi/pdf/10.2514/1.G002751
Reference18 articles.
1. Closed-Loop Optimization of Guidance Gain for Constrained Impact
2. A Non-Switching Guidance Law with Terminal Constraints
3. Terminal Impact Angle Constraint Guidance With Dual Sliding Surfaces and Model-Free Target Acceleration Estimator
4. Range-to-go weighted optimal guidance with impact angle constraint and seeker's look angle limits
5. Biased proportional navigation with exponentially decaying error for impact angle control and path following
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