Sensitivity of mars entry navigation errors to sensed acceleration threshold

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Bishop, Robert H ^a   Crain, Timothy P ^b   Azimov, Dilmurat M ^a  

^a The University of Texas at Austin   (United States)

^b NASA JOHNSON SPACE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION THRESHOLD; FILTER PERFORMANCE; MONTE CARLO EXPERIMENTS; NAVIGATION FILTERS; NAVIGATION PERFORMANCE; PROCESS BENEFITS; SUPERSONIC PARACHUTE; THRESHOLD LEVELS;

ERRORS; NAVIGATION; PARACHUTES; SEPARATION; STATE ESTIMATION;

ACCELERATION;

EID: 84896693790     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Bishop, R.H., and Crain,II P.T., "Precision entry navigation dead-reckoning error analysis: Theoreti- cal foundations of the continuous case," Technical report, The University of Texas at Austin and NASA Johnson Space Center, May 2001.
2. Bishop, R.H., and Azimov, D.M., "Mars Science Laboratory EDL: Sensed acceleration threshold studies," Technical report, The University of Texas at Austin and NASA Johnson Space Center, December 2002.
3. Gelb, A., ets., Applied Optimal Estimation, Chapters 7 and 8, The M.I.T. Press, Cambridge, Mas- sachusetts, and London, England, 1974, pp.229-315.
4. "Sort 8.1. User's guide," Sections 2.10, 2.12, 2.24., Systems Development Branch. Systems Engineering Division. NASA Johnson Space Center. 2002.