| | Location: Home» Jet Engines » Subjects » Robust, Multivariable, Quantitative Design of an Adaptive Model-Based Control for Jet Engines | |
|
|
Robust, Multivariable, Quantitative Design of an Adaptive Model-Based Control for Jet Engines | 
 enlarge | Publisher: Storming Media
Category: Book
Buy New: $42.95
Sales Rank: 5454654
Media: Spiral-bound
Pages: 157
ISBN: 1423553071
EAN: 9781423553076
ASIN: 1423553071
Publication Date: 1998
Availability: Usually ships in 1-2 business days
Shipping: Expedited shipping available
Shipping: International shipping available
Condition: Please note that this is a report or document and is not a book, per se. It is 157 pages long and is Velobound in a soft linen cover. This technical report was sponsored by the Pentagon and is provided in the best form available to the government. Sometimes our report quality is picture perfect and in color; other times, particularly for older reports, extensive black-and-white photocopying has degraded the quality. If you have any questions about quality of a particular report, please ask and we would be happy to describe it in more detail.
| |
| Editorial Reviews:
Product Description
This is a AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH PROPULSION DIRECTORATE report procured by the Pentagon and made available for public release. It has been reproduced in the best form available to the Pentagon. It is not spiral-bound, but rather assembled with Velobinding in a soft, white linen cover. The Storming Media report number is A596863. The abstract provided by the Pentagon follows: The robust design of a model-based control system for a single-spool gas turbine engine is presented. The overall objective of this work is to develop a robust, quantitative design methodology that allows the turbine engine control system engineer the ability to control variables that can not be directly measured. The study makes use of the model-based control structure that is of current interest within the turbine engine control community. Then the concept of robustness is added to the model-based control structure to ensure satisfactory operation of the turbine engine throughout the flight envelope.
|
|
|
| |
|
