Generalized Impact Time and Angle Control Via Look-Angle Shaping
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
2. Aselsan, Inc., 06750 Ankara, Turkey
3. Technical University of Munich, 85748 Munich, Germany
Funder
China Scholarship Council
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.G003765
Reference22 articles.
1. Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories
2. Indirect Impact-Angle-Control Against Stationary Targets Using Biased Pure Proportional Navigation
3. Optimal Guidance Laws with Terminal Impact Angle Constraint
4. Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint
5. Polynomial Guidance Laws Considering Terminal Impact Angle and Acceleration Constraints
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