A Nonlinear Suboptimal Guidance Law with 3D Impact Angle Constraints for Ground Targets-Reference-Cited by-同舟云学术

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A Nonlinear Suboptimal Guidance Law with 3D Impact Angle Constraints for Ground Targets

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
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Author:

Oza Harshal¹,Padhi Radhakant¹

Affiliation:

1. Indian Institute of Science

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-8185

Reference22 articles.

1. AIAA Tactical Missile Series;Zarchan P.,1994

2. Optimal Guidance Laws with Terminal Impact Angle Constraint

3. Impact Time and Angle Guidance with Sliding Mode Control

4. Guidance law to control impact time and angle

5. Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A trajectory shaping guidance law with field-of-view angle constraint and terminal limits;Journal of Systems Engineering and Electronics;2022-04

2. Detailed Analysis of Nonlinear Impact Angle Guidance Law via Controlling Line-Of-Sight Dynamics;AIAA Scitech 2019 Forum;2019-01-06

3. Impact Angle Guidance Law via Controlling Line-of-Sight Dynamics;2018 AIAA Guidance, Navigation, and Control Conference;2018-01-07

4. Nonlinear Impact Angle Control Guidance Law for Stationary Targets;AIAA Guidance, Navigation, and Control Conference;2016-01-01

5. Partial Integrated Guidance and Control with Impact Angle Constraints;Journal of Guidance, Control, and Dynamics;2015-05

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