Abstract
Optimal control techniques have been applied to the problem of conserving fuel in C-141A aircraft. Numberical results form the basis for designing an on-board energy management system, which can automatically command fuel-optimal climb, cruise, and descent flight paths for a majority of this aircraft's missions.
Original language | English (US) |
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Pages (from-to) | 464-471 |
Number of pages | 8 |
Journal | IEEE Transactions on Aerospace and Electronic Systems |
Volume | AES-12 |
Issue number | 4 |
DOIs | |
State | Published - Jul 1976 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Electrical and Electronic Engineering