|
Uniform System for the Rapid Prototyping and Testing of Controllers for Unmanned Aerial Vehicles | 
 enlarge | Publisher: Storming Media
Category: Book
Buy New: $29.95
Media: Spiral-bound
Pages: 97
ISBN: 1423574613
EAN: 9781423574613
ASIN: 1423574613
Publication Date: 1996
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 97 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 NAVAL POSTGRADUATE SCHOOL MONTEREY CA 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 A283223. The abstract provided by the Pentagon follows: The field of control systems has witnessed an explosion in state- space techniques addressing a variety of critical design issues facing control engineers today. Modem computational tools, such as the MATRIX(x) Product Family developed by Integrated Systems Incorporated, allow the designer to quickly design, test and implement control systems based on these state-space techniques. These new computing advances shorten the time required to complete a control design from a few years to a few months. However, as the design process progressed new inputs and outputs were required, which usually resulted in a confusing mess of connections that were hard to follow. Therefore, a universal system was needed that could be used on any controller design to aid in the understanding and tracking of the controller's inputs and outputs. A description of this system is given along with a detailed step by step process on how it was implemented on a Unmanned Air Vehicle (UAV).
|
|
|
| |
