Near optimal re-entry guidance law using inverse problem approach
Author:
Affiliation:
1. Aerospace Engineering Department, Amirkabir University of Technology, Tehran, Iran
Publisher
Informa UK Limited
Subject
Applied Mathematics,Computer Science Applications,General Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/17415970701256437
Reference31 articles.
1. Guidance law for planar hypersonic descent to a point
2. Guidance law for hypersonic descent to a point
3. Inverse dynamics approach to trajectory optimization for an aerospace plane
4. Explicit guidance along an optimal space curve
5. Guidance Algorithm Design: A Nonlinear Inverse Approach
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