Apollo-derived mars precision lander guidance

23rd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1998, Pages 1-18

  Carman, Gilbert L ^a   Ives, Dallas G ^a   Geller, David K ^b  

^a NASA JOHNSON SPACE CENTER   (United States)

^b CHARLES STARK DRAPER LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALTITUDE CONTROL; CRASHWORTHINESS; ELECTRONIC GUIDANCE SYSTEMS; LANDING; LUNAR LANDING; NAVIGATION; SPACECRAFT LANDING;

CAPABILITY ENVELOPES; CONTROL EQUATIONS; ENTRY GUIDANCE; ENTRY VELOCITY; GUIDANCE ALGORITHM; PRECISION LANDING; REFERENCE TRAJECTORIES; TARGET SELECTION;

ALGORITHMS;

EID: 84983152455     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Mars Surveyor Program: 2001 Lander Mission Proposal Information Package, 30 June 1997.
2. P. E. Moseley. "The Apollo Entry Guidance: A review of the mathematical development and its operational characteristics," TRW Note No. 69-FMT-791, December 1, 1969.
3. Gerald L. Hunt. "Apollo Reentry Guidance and Navigation equations and flow logic," MSC Internal Note No. 65-FM-157, December 13, 1965.
4. Claude A. Graves and Jon C. Harpold. "Apollo Experience report: Mission Planning for Apollo reentry," MSC Internal Note No. 70-FM-155, October 5, 1970.
5. Arthur E. Bryson, Yu-Chi Ho, "Applied Optimal Control," Hemisphere Publishing Corporation, 1975.