This document is intended to provide the specifications and requirements for a flight control system design challenge. The response to the challenge will involve documenting whether the particular design has met the stated requirements through analysis and computer simulation. The response should be written in the general format of a technical publication with corresponding length limits, e.g., an approximate maximum length of 45 units, with each full-size figure and double-spaced typewritten page constituting one unit.
2002 Controls Design Challenge
2002-01-01
Miscellaneous
No indication
English
Controls Design Challenge: A Variable Structure Approach
Online Contents | 1994
|Aircraft Model for the AIAA Controls Design Challenge
Online Contents | 1994
|Aircraft Model for the Aiaa Controls Design Challenge
NTIS | 1991
|Aircraft model for the AIAA controls design challenge
AIAA | 1994
|