NASA Technical Reports Server (NTRS) 19780015197: The Dynamics And Control Of Large Flexible Space Structures. Part B: Development Of Continuum Model And Computer Simulation - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19780015197: The Dynamics And Control Of Large Flexible Space Structures. Part B: Development Of Continuum Model And Computer Simulation" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19780015197: The Dynamics And Control Of Large Flexible Space Structures. Part B: Development Of Continuum Model And Computer Simulation” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19780015197: The Dynamics And Control Of Large Flexible Space Structures. Part B: Development Of Continuum Model And Computer Simulation
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19780015197
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"NASA Technical Reports Server (NTRS) 19780015197: The Dynamics And Control Of Large Flexible Space Structures. Part B: Development Of Continuum Model And Computer Simulation" Description:
The Internet Archive:
The equations of motion of an arbitrary flexible body in orbit were derived. The model includes the effects of gravity with all its higher harmonics. As a specific example, the motion of a long, slender, uniform beam in circular orbit was modelled. The example considers both the inplane and three dimensional motion of the beam in orbit. In the case of planar motion with only flexible vibrations, the pitch motion is not influenced by the elastic motion of the beam. For large values of the square of the ratio of the structural modal frequency to the orbital angular rate the elastic motion was decoupled from the pitch motion. However, for small values of the ratio and small amplitude pitch motion, the elastic motion was governed by a Hill's 3 term equation. Numerical simulation of the equation indicates the possibilities of instability for very low values of the square of the ratio of the modal frequency to the orbit angular rate. Also numerical simulations of the first order nonlinear equations of motion for a long flexible beam in orbit were performed. The effect of varying the initial conditions and the number of modes was demonstrated.
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