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A Control Law Design Method Facilitating Control Power%2c Robustness%2c Agility%2c And Flying Qualities Tradeoffs%2c Craft by Murphy%2c Patrick C.
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1NASA Technical Reports Server (NTRS) 19990025985: A Control Law Design Method Facilitating Control Power, Robustness, Agility, And Flying Qualities Tradeoffs: CRAFT
By NASA Technical Reports Server (NTRS)
A multi-input, multi-output control law design methodology, named "CRAFT", is presented. CRAFT stands for the design objectives addressed, namely, Control power, Robustness, Agility, and Flying Qualities Tradeoffs. The methodology makes use of control law design metrics from each of the four design objective areas. It combines eigenspace assignment, which allows for direct specification of eigenvalues and eigenvectors, with a graphical approach for representing the metrics that captures numerous design goals in one composite illustration. Sensitivity of the metrics to eigenspace choice is clearly displayed, enabling the designer to assess the cost of design tradeoffs. This approach enhances the designer's ability to make informed design tradeoffs and to reach effective final designs. An example of the CRAFT methodology applied to an advanced experimental fighter and discussion of associated design issues are provided.
“NASA Technical Reports Server (NTRS) 19990025985: A Control Law Design Method Facilitating Control Power, Robustness, Agility, And Flying Qualities Tradeoffs: CRAFT” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19990025985: A Control Law Design Method Facilitating Control Power, Robustness, Agility, And Flying Qualities Tradeoffs: CRAFT
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19990025985: A Control Law Design Method Facilitating Control Power, Robustness, Agility, And Flying Qualities Tradeoffs: CRAFT” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - CONTROL THEORY - EIGENVALUES - EIGENVECTORS - FLIGHT CONTROL - THRUST VECTOR CONTROL - FIGHTER AIRCRAFT - AERODYNAMIC CHARACTERISTICS - ANGLE OF ATTACK - TRANSFER FUNCTIONS - DAMPING - Murphy, Patrick C. - Davidson, John B.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19990025985
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The book is available for download in "texts" format, the size of the file-s is: 51.59 Mbs, the file-s for this book were downloaded 70 times, the file-s went public at Sat Oct 15 2016.
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