Further improvements to a hybrid method for launch vehicle ascent trajectory optimization-Reference-Cited by-同舟云学术

Further improvements to a hybrid method for launch vehicle ascent trajectory optimization

Published:2000-08-14 Issue: Volume: Page:
ISSN:
Container-title:18th Applied Aerodynamics Conference
language:
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Author:

Calise Anthony¹,Tandon Sunil²,Young Daniel²,Kim Sungwan²

Affiliation:

1. Georgia Inst. of Technology, Atlanta

2. Boeing Co., Huntington Beach, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4261

Reference8 articles.

1. Gath, P.P., Calise, A.J. "Optimization of Launch VehicleAscent Trajectories with Path Constraints and Coast Arcs,"AIAA-99-4308 (to appear in Journal of Guidance, Control, and Dynamics).

2. Optimal Analytic Multiburn Trajectories

3. Direct trajectory optimization using nonlinear programming and collocation

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

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