Verification of a Fully Numerical Entry Guidance Algorithm-Reference-Cited by-同舟云学术

Verification of a Fully Numerical Entry Guidance Algorithm

Published:2017-02 Issue:2 Volume:40 Page:230-247
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Lu Ping¹,Brunner Christopher W.²,Stachowiak Susan J.³,Mendeck Gavin F.³,Tigges Michael A.³,Cerimele Christopher J.³

Affiliation:

1. San Diego State University, San Diego, California 92182-1308

2. Odyssey Space Research, Houston, Texas 77058

3. NASA Johnson Space Center, Houston, Texas 77058

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000327

Reference39 articles.

1. MoseleyP. E. “The Apollo Entry Guidance: A Review of the Mathematical Development and its Operational Characteristics,” TRW Note No. 69-FMT-791, Houston, TX, Dec. 1969.

2. DiCarloJ. L. “Aerocapture Guidance Methods for High-Energy Trajectories,” S.M. Thesis, Department of Aeronautics and Astronautics, MIT, 2003.

3. BairstowS. H. “Reentry Guidance with Extended Range Capability for Low L/D Spacecraft,” S. M. Thesis, Department of Aeronautics and Astronautics, MIT, Feb. 2006.

4. A Comparison of Two Orion Skip Entry Guidance Algorithms

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