End-to-End Performance Optimization for High-Speed Ascent–Entry Missions-Reference-Cited by-同舟云学术

End-to-End Performance Optimization for High-Speed Ascent–Entry Missions

Published:2021-12-16 Issue: Volume: Page:1-18
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Miller Alexander T.¹,Rao Anil V.¹^ORCID

Affiliation:

1. University of Florida, Gainesville, Florida 32611

Funder

National Defense Science and Engineering Graduate Fellowship

Division of Mathematical Sciences

Office of Naval Research

Division of Civil, Mechanical and Manufacturing Innovation

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.A35171

Reference47 articles.

1. The Optimization of Trajectories

2. Improvement of missile and space vehicle accuracy by trajectory optimization.

3. Design and Evaluation of a Three-Dimensional Optimal Ascent Guidance Algorithm

4. MarklA. W. “An Initial Guess Generator for Launch and Reentry Vehicle Trajectory Optimization,” Doctoral Thesis, Universität Stuttgart, Germany, 2001. 10.18419/opus-3655

5. Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast Arcs

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