Heading Error Shaping Guidance Laws Using Generalized Finite-Time Convergence Error Dynamics-Reference-Cited by-同舟云学术

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Heading Error Shaping Guidance Laws Using Generalized Finite-Time Convergence Error Dynamics

Published:2024-06 Issue:3 Volume:60 Page:3192-3208
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Jeong Eui-Taek¹^ORCID,Wang Pengyu¹^ORCID,He Shaoming²^ORCID,Kim Tae-Hun³^ORCID,Lee Chang-Hun¹^ORCID

Affiliation:

1. Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, South Korea

2. School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China

3. Department of Aerospace Engineering, Korea Aerospace University, Goyang, South Korea

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/7/10552647/10419004.pdf?arnumber=10419004

Reference43 articles.

1. Time-to-go weighted optimal guidance with impact angle constraints

2. Optimality of Linear Time-Varying Guidance for Impact Angle Control

3. Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint

4. Range-to-go weighted optimal guidance with impact angle constraint and seeker's look angle limits

5. New Look-Angle Tracking Guidance Strategy for Impact Time and Angle Control

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