Impact Angle Guidance Using Computationally Enhanced State-Dependent Differential Riccati-Equation Scheme

Author:

Lin Li-Gang1,Wu Ruei-Syuan1,Yeh Chih-Ting2,Xin Ming3ORCID

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

This study considers the latest three-dimensional impact angle guidance based on the state-dependent differential Riccati-equation (SDDRE) scheme, and it presents novel theories that efficiently guarantee the SDDRE’s applicability and largely reduce the computational burden. The unified applicability analysis completely categorizes the state space in terms of a simple equivalent condition, where all the inapplicable cases (leading to implementation breakdowns) are newly discovered and efficiently resolved. The condition almost removes the tedious online checking routine, which accounts for the dominant effort as endorsed by complexity analysis and practical validations. Moving forward to a general scope, we analyze the computational complexity of such an SDDRE controller: first subject to the MATLAB® framework and then the state-of-the-art enhancements, where the latter come from the best performance among extensive trials. Finally, numerical and hardware experiments (notably, microcontroller and field-programmable gate array) strengthen the confidence in the analytical findings, and they enrich the value in robustness and generality that benefit more guidance or control systems.

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

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