Article ID Journal Published Year Pages File Type
8058003 Aerospace Science and Technology 2018 13 Pages PDF
Abstract
This paper investigates a robust virtual target guidance algorithm for the fixed-trim Maneuverable Reentry Vehicle. The vehicle is faced with multi-constraints including terminal and process constraints. A virtual target integrated spinning guidance law is developed, and the virtual target's capability of handling multi-constraints is validated through analysis. A parametric optimization approach is proposed to determine the virtual target motion. The approach is further developed into a robustness optimization approach, which introduces a measurement of robustness into the optimization and estimates the measurement by Monte Carlo sampling. Illustrative results indicate the constraint-handling capability of the virtual target and the robustness of the proposed guidance algorithm.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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