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Guidance and Navigation Challenges for a Mars Ascent VehicleThis work presents studies and analysis in support of a Mars Ascent Vehicle as part of a Martian Sample Return campaign. The vehicle design has been ongoing, with rapid development of a 6 Degree of Freedom simulation to capture full vehicle dispersions and integrated performance of vehicle, guidance, navigation and control. The maturation of this simulation is presented to provide an overview of its capabilities added over the past year of effort. The results describe in detail guidance algorithm development to increase the system’s robustness to thrust sensitivities. Navigation performance and sensitivity analysis are included to describe the capabilities of the current design as well as identify primary drivers of insertion performance. Lastly, integrated vehicle 6DOF statistical results are presented to provide insight into the nominal performance of the current vehicle and insight into system-level drivers. Future work is described to outline the continuing maturation and development of the MSR MAV ascent vehicle.
Document ID
20200002335
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Anzalone, Evan ORCID
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Erickson, Dane
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Everett, Jason
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Powers, Joey
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
April 13, 2020
Publication Date
March 7, 2020
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M20-7873
Report Number: M20-7873
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 7, 2020
End Date: March 14, 2020
Sponsors: Institute of Electrical and Electronics Engineers (IEEE)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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