Precision Landing at Mars Using Discrete-Event Drag Modulation-Reference-Cited by-同舟云学术

Precision Landing at Mars Using Discrete-Event Drag Modulation

Published:2014-01 Issue:1 Volume:51 Page:128-138
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Putnam Zachary R.¹,Braun Robert D.¹

Affiliation:

1. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32633

Reference25 articles.

1. Mars Exploration Entry, Descent, and Landing Challenges

2. Aerodynamic Challenges for the Mars Science Laboratory Entry Descent and Landing

3. CiancioloA. M. D.DavisJ. L.EngelundW. C.KomarD. R.QueenE. M.SamarehJ. A.WayD. W.ZangT. A.MurchJ. G.KrizanS. A.OldsA. D.PowellR. W.ShidnerJ. D.KinneyD.McGuireM. K.ArnoldJ. O.CovingtonM. A.SostaricR. R.ZumwaltC. H.LlamaE. G.” Entry, Descent and Landing Systems Analysis Study,” NASA TM-2011-217055, Feb. 2011.

4. LevyL. L. “The Use of Drag Modulation to Limit the Rate at Which Deceleration Increases During Nonlifting Entry,” NASA TN-D-1037, Sept. 1961.

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