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Massachusetts Institute of Technology

Optimization study of a trans-Atlantic abort for the U.S. space shuttle using a pseudospectral Legendre method

Abstract

dc:description.abstract

The problem of performance optimization for a trans-Atlantic shuttle abort is considered. At five points during the second stage of ascent, a failure of a main engine occurs, which necessitates an abort from the nominal mission. The abort trajectories generated initiate from the current state at the time of abort and terminate at the TAEM interface for a landing site. The abort trajectories consist of three regimes, or phases of flight, and each phase has a different dynamic model governing the motion of the vehicle. To ensure a solution is obtained for each abort, additional constraints on the vehicle are formulated as soft constraints in the penalty function. In particular, the third phase cost functional consists of a weighted combination of heating rate, dynamic pressure and sensed acceleration. Thus, the problem formulation is one of a multiple phase optimal control problem. A Pseudospectral Legendre Method is used to discretized the optimal control problem into a nonlinear programming problem, which is then solved using a sparse nonlinear optimizer. The first study conducted compares the trajectories generated to each landing site for various combinations of third phase cost functional weighting factors. A cost calculation is developed to compare each optimized abort trajectory. The second study evaluates the significance of the improvements due to the chosen weighting factor combination with that of an entry aerodynamic model uncertainty.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2003

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Taylor, Christine P. (Christine Pia), 1979-
Advisor dc:contributor.advisor
  • Anil V. Rao.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/42083
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/42083

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
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citation

Taylor, Christine P. (Christine Pia), 1979-. Optimization study of a trans-Atlantic abort for the U.S. space shuttle using a pseudospectral Legendre method. Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/42083