Impact angle constraint guidance law using fully-actuated system approach-Reference-Cited by-同舟云学术

Impact angle constraint guidance law using fully-actuated system approach

Published:2023-05 Issue: Volume:136 Page:108220
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chen Shiwei^ORCID,Wang Wei,Fan Junfang^ORCID,Ji Yi

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. Switched-gain guidance for impact angle control under physical constraints;Tekin;J. Guid. Control Dyn.,2015

2. Minimum-effort intercept angle guidance with multiple-obstacle avoidance;Kumar;J. Guid. Control Dyn.,2018

3. Guidance strategy with impact angle constraint based on pure proportional navigation;Li;Acta Aeronaut. Astronaut. Sin.,2020

4. Capture region of RTPN guidance law against arbitrarily maneuvering targets;Bai;Acta Aeronaut. Astronaut. Sin.,2020

5. Parameter optimization of proportional navigation guidance for 2D trajectory correction projectile with fixed canard;Cao;Acta Aeronaut. Astronaut. Sin.,2021

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