Postflight Assessment of Mars 2020 Entry, Descent, and Landing Simulation

Author:

Dutta Soumyo1ORCID,Way David W.1,Zumwalt Carlie H.1,Blette David J.1

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Abstract

On 18 February 2021, the Mars 2020 Perseverance rover and Ingenuity helicopter successfully landed inside Jezero Crater. At 1026 kg, Perseverance is the largest, most sophisticated rover ever delivered to another planet. This event marked the ninth successful landing and fifth rover to be delivered at Mars. The Program to Optimize Simulated Trajectories II, a trajectory simulation tool, was the prime entry, descent, and landing performance simulation for Mars 2020. This paper presents comparisons between the flight telemetry and the simulation predictions. In general, approximately 90% of the as-flown values were within [Formula: see text] (standard deviations) of the preflight simulation predictions, and the anomalies are discussed in the paper. These comparisons are important in order to understand how each of the individual models and the integrated simulation as a whole performed. This information is fed forward to future missions, which benefit from knowing where additional resources or studies are needed and where uncertainties may be reduced to enable improved performance.

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Reference19 articles.

1. MustardJ.AdlerM.AllwoodA.BassD.BeatyD.BellJ. IIIBrinckerhoffW.CarrM.Des MaraisD.DrakeB.et al. “Report of the Mars 2020 Science Definition Team,” Mars Exploration Program Analysis Group (MEPAG) TR-CL#13-2464, Jet Propulsion Lab., Pasadena, CA, 2013, http://mepag.jpl.nasa.gov/reports/MEP/Mars_2020_SDT_Report_Final.pdf [retrieved 29 Oct. 2015].

2. Comparison of the Effects of Velocity and Range Triggers on Trajectory Dispersions for the Mars 2020 Mission

3. Mars Entry, Descent, and Landing Instrumentation 2 Trajectory, Aerodynamics, and Atmosphere Reconstruction

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