Onboard near-optimal climb-dash energy management

This paper studies optimal and near-optimal trajectories of high-performance aircraft in symmetric flight. Onboard, real-time, near-optimal guidance is considered for the climb-dash mission, using some of the boundary-layer structure and hierarchical ideas from singular perturbations. In the case of...

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Veröffentlicht in:Journal of guidance, control, and dynamics control, and dynamics, 1985-05, Vol.8 (3), p.320-324
Hauptverfasser: WESTON, A, CLIFF, G, KELLEY, H
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container_title Journal of guidance, control, and dynamics
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creator WESTON, A
CLIFF, G
KELLEY, H
description This paper studies optimal and near-optimal trajectories of high-performance aircraft in symmetric flight. Onboard, real-time, near-optimal guidance is considered for the climb-dash mission, using some of the boundary-layer structure and hierarchical ideas from singular perturbations. In the case of symmetric flight, this resembles neighborhood-optimal guidance using energy-to-go as the running variable. However, extension to three-dimensional flight is proposed, using families of nominal paths with heading-to-go as the additional running variable. Some computational results are presented for the symmetric case.
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source NASA Technical Reports Server; Alma/SFX Local Collection
subjects Aerospace engineering
Aircraft
Aircraft Design, Testing And Performance
aircraft engineering
Algorithms
Altitude
Energy management
Energy modeling
flight control systems
guidance and control systems
optimal control
title Onboard near-optimal climb-dash energy management
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