Compuation of Real-Time-Control in Aerospace Applications by Multiple Shooting Procedures View Full Text


Ontology type: schema:Chapter     


Chapter Info

DATE

1974

AUTHORS

R. Bulirsch , H.-W. Branca

ABSTRACT

Extended AbstractLet the problem of optimal control be defined as (1)\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$ {\rm{\dot \eta = \Phi }}\left( {{\rm{t,\eta ,u}}} \right){\rm{ , }}{{\rm{t}}_{\rm{o}}} \le {\rm{t}} \le {{\rm{t}}_{\rm{e}}} $$\end{document} with boundary conditions for the state variable η(t) at t = to and t = te, te fixed or free, u(t) is the control; the quantity to be optimized is denoted by Ф(te, η(te)). More... »

PAGES

49-50

Book

TITLE

Stiff Differential Systems

ISBN

978-1-4684-2102-6
978-1-4684-2100-2

Identifiers

URI

http://scigraph.springernature.com/pub.10.1007/978-1-4684-2100-2_4

DOI

http://dx.doi.org/10.1007/978-1-4684-2100-2_4

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1037868457


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