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) |
|---|---|
| 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