Abdallah et al., 2013 - Google Patents
Measuring aircraft nonlinearity across aerodynamic attitude flight envelopeAbdallah et al., 2013
- Document ID
- 7328477183057123167
- Author
- Abdallah A
- Newman B
- Omran A
- Publication year
- Publication venue
- AIAA Atmospheric Flight Mechanics (AFM) Conference
External Links
Snippet
HE operational range of an aircraft is commonly described by the symmetric level speed- altitude envelope. This envelope is used for design requirement specification and satisfication, dynamic analysis over differing flight phases, control synthesis using …
- 230000003068 static 0 abstract description 22
Classifications
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- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5086—Mechanical design, e.g. parametric or variational design
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