Impact Angle Guidance Using Computationally Enhanced State-Dependent Differential Riccati-Equation Scheme
Author:
Affiliation:
1. National Central University, Taoyuan 32001, Taiwan, Republic of China
2. Taiwan Semiconductor Manufacturing Company, Ltd., Hsinchu 30075, Taiwan, Republic of China
3. University of Missouri–Columbia, Columbia, Missouri 65211
Abstract
Funder
National Science and Technology Council, Taiwan
Max-Planck-Gesellschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35624
Reference38 articles.
1. Optimal Guidance and Control of a Low-Altitude Skid-to-Turn Vehicle
2. Parallel-Structured Newton-Type Guidance by Using Modified Chebyshev–Picard Iteration
3. Nonlinear Optimal Impact-Angle-Constrained Guidance with Large Initial Heading Error
4. Lead-Angle-Based Three-Dimensional Guidance for Angle-Constrained Interception
5. Two-Stage Guidance Law With Constrained Impact via Circle Involute
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