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Structural dynamics, stability, and control of helicopters
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kraige, L. G. Meirovitch, L. Hale, A. L. |
| Copyright Year | 1976 |
| Description | The dynamic synthesis of a helicopter is reported. The method of approach is a variation of the component mode synthesis in the sense that it regards the aircraft as an assemblage of interconnected substructures. The equations of motion are derived in general form by means of the Lagrangian formulation in conjunction with an orderly kinematical procedure that takes into account the superposition of motion of various substructures, thus circumventing constraint problems. |
| File Size | 4849495 |
| Page Count | 98 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760019103 |
| Archival Resource Key | ark:/13960/t6wx25n7j |
| Language | English |
| Publisher Date | 1976-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Dynamic Structural Analysis Substructures Airframes Lagrange Coordinates Vibration Mode Mathematical Models Aerodynamic Stability Equations of Motion Helicopter Design Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
