Crew exploration vehicle launch abort controller performance analysis

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 3, Issue , 2007, Pages 2559-2580

  Sparks Jr , Dean W ^a,b   Raney, David L ^a,b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Dynamic Systems and Control Branch   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CREW MODULE (CM); LAUNCH ABORT SYSTEM (LAS); PERFORMANCE ANALYSIS;

AUTOMOTIVE ENGINEERING; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); MONTE CARLO METHODS; PARAMETER ESTIMATION; TRAJECTORIES;

CONTROL EQUIPMENT;

EID: 37249087849     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. McCarthy, J. F. JR., Dodds, J. Ian, Crowders, R. S., "Development of the Apollo Launch Escape System", J. Spacecraft, Vol. 5, No. 8, p.927, North American Rockwell Corporation, Downey, CA, Aug. 1968.
2. Users Guide for the ANTARES Simulation, Engineering Directorate, Aerosciences and Flight Mechanics Division. Johnson Space Center, Mar., 2007.
3. Vetter, Keith, The Trick Design Document - Trick 2004.0 Release. Titan Corporation, Aug. 2004.
4. Justus, C. G., Johnson, D. L., "The NASA/MSFC Global Reference Atmospheric Model - 1999 Version (GRAM-99)", NASA-TM-1999-209630, May 1999.
5. Brown, S. C., "150 Per Month Jimsphere Wind Speed Profiles for Aerospace Vehicle Design Capability Studies, Location: Kennedy Space Center", MSFC-ES81, Feb., 1978.