Minimum-fuel attitude control of a spacecraft by an extended method of steepestdescent

DOI10.1016/0020-7462(68)90029-2zbMath0167.39303OpenAlexW2042255476MaRDI QIDQ2530841

K. A. Hales, B. O. Lange, Irmgard Flügge-Lotz

Publication date: 1968

Published in: International Journal of Non-Linear Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0020-7462(68)90029-2

zbMATH Keywords

ordinary differential equations

Related Items (2)

Computational and approximate methods of optimal control ⋮ On optimal control problems with discontinuities

This page was built for publication: Minimum-fuel attitude control of a spacecraft by an extended method of steepestdescent