Design and Evaluation of an Acceleration Guidance Algorithm for Entry-Reference-Cited by-同舟云学术

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Design and Evaluation of an Acceleration Guidance Algorithm for Entry

Published:2003-06-22 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
Short-container-title:

Author:

Saraf Amitabh¹,Leavitt James¹,Chen David¹,Mease Kenneth¹

Affiliation:

1. University of California Irvine

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5737

Reference16 articles.

1. Normalized Energy

2. HAC Point Fig.

Cited by 4 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. Introduction;Steady Glide Dynamics and Guidance of Hypersonic Vehicle;2020-11-08

2. A trajectory generation framework for modeling spacecraft entry in MDAO;Acta Astronautica;2016-04

3. Survey of planetary entry guidance algorithms;Progress in Aerospace Sciences;2014-07

4. Dynamic Lateral Entry Guidance Logic;AIAA Guidance, Navigation, and Control Conference and Exhibit;2004-06-22

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