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Virginia Polytechnic Institute and State University

Singular trajectories in airplane cruise-dash optimization

Abstract

dc:description.abstract

The problem of determining cruise-dash trajectories is examined for the case of time-fuel optimization using a linear combination of time and fuel as the performance index. These trajectories consist of a transient arc followed by a steady-state arc. For cases where the steady-state arc is flown with full throttle the associated skeletal transient trajectories are also flown with full throttle, and approach the cruise-dash points monotonically in an asymptotic fashion. When the steady-state arc is flown at an intermediate throttle setting, the transient trajectories follow a singular control law and exhibit a complex structure that is different from the full-throttle transients. Singular transients in the vicinity of singular cruise-dash points are confined to a bounded singular surface. In state-space these trajectories trace out asymptotic spirals on the singular surface as they approach the steady-state arc. If the initial operating point lies outside the singular surface, then the transient trajectories are composites consisting of a full-throttle or zero-throttle segment flown until the singular surface is met, followed by a singular segment that fairs into the cruise-dash point. Addressing the question of optimality of the steady-state arc, it was found that although steady-state cruise fails a Jacobi-type condition, steady-state cruise-dash can satisfy this condition if the emphasis on time is sufficiently large. The outcome of the Jacobi-type test appears to be connected with the eigenstructure of the linearized state-adjoint system.

Degree

thesis:*
Name thesis:degree_name
PH. D.
Level thesis:degree_level
doctoral
Discipline thesis:degree_discipline
Aerospace Engineering
Department dc:contributor.department
Aerospace Engineering
Grantor dc:publisher
Virginia Polytechnic Institute and State University
Year dc:date.issued
1987

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Bilimoria, Karl D.
Chair dc:contributor.committeechair
  • Cliff, Eugene M.
Committee members dc:contributor.committeemember
  • Kelley, Henry J.
  • Lutze, Frederick H.
  • Stalford, Harold L.
  • Marchman, James F.

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en_US

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/10919/76506
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/76506

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Bilimoria, Karl D.. Singular trajectories in airplane cruise-dash optimization. doctoral thesis, Virginia Polytechnic Institute and State University, 1987. http://hdl.handle.net/10919/76506