GN&C Design Overview and Flight Test Results from NASA's Max Launch Abort System (MLAS)-Reference-Cited by-同舟云学术

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GN&C Design Overview and Flight Test Results from NASA's Max Launch Abort System (MLAS)

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

Author:

Dennehy Cornelius¹,Lanzi Raymond²,Ward Philip²

Affiliation:

1. NASA Goddard Space Flight Center

2. NASA Wallops Flight Facility

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-8432

Reference5 articles.

1. NASA Engineering and Safety Center (NESC) GN&C Technical Discipline Team (TDT): Its Purpose, Practices and Experiences

2. JavadNavigationSystems,Inc."JNS100-GGOperator‟sManual,"December2006, http://www.javad.com/jns/index.html?/jns/support/manuals.html [cited 2/15/2008].

3. J.Lanzi,"Port-O-SimObjectSimulationApplication,"NASATechBriefs,September2009, http://www.embeddedtechmag.com/component/content/article/5668 [cited9/10/2008].

Cited by 2 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 Proposed Ascent Abort Flight Test for the Max Launch Abort System;AIAA Atmospheric Flight Mechanics Conference;2016-01-01

2. Flight Performance Feasibility Studies for the Max Launch Abort System;AIAA Atmospheric Flight Mechanics (AFM) Conference;2013-08-15

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