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Toward Improved Landing Precision on MarsMars landers to date have flown ballistic entry trajectories with no trajectory control after the final maneuver before entry. Improvements in landing accuracies (from approx.150 km from the target for Mars Pathfinder to approx.30-40 km for MER and Phoenix) have been driven by approach navigation improvements. MSL will fly the first guided-entry trajectory to Mars, further improving accuracy to approx.10-12 km from the target.
Document ID
20110020614
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/41892
Authors
Wolf, Aron A. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Acikmese, Behcet (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cheng, Yang (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Casolica, Jordi (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Carson, John M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ivanov, Mark C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
March 5, 2011
Publication Information
ISBN: 978-1-4244-7351-9
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IEEEAC Paper 1209
Report Number: IEEEAC Paper 1209
ISBN: 978-1-4244-7351-9
Meeting Information
Meeting: 2011 IEEE Aersopace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 5, 2011
End Date: March 12, 2011
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Other
Keywords
powered descent guidance
pinpoint landing
terrain relative navigation
precision landing

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