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Issues in modeling and controlling the scole configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Reddy, A. S. S. R. Diarra, Cheick Modibo Li, Feiyue Bainum, Peter M. |
| Copyright Year | 1987 |
| Description | The parametric study of the in-plane Spacecraft Control Laboratory Experiment (SCOLE) system, the Floquet Stability Analysis, and three dimensional formulations of the SCOLE system dynamics are examined. Control issues are discussed, such as: control of large structures with delayed input in continuous time; control with delayed input in discrete time; control law design for SCOLE using Linear Quadratic Gaussian (LQC)/TRR technique; and optimal torque control for SCOLE slewing maneuvers. |
| File Size | 1179144 |
| Page Count | 57 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870008389 |
| Archival Resource Key | ark:/13960/t9c58h34x |
| Language | English |
| Publisher Date | 1987-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Slewing Spacecraft Maneuvers Boundary Value Problems Vibration Damping Linear Quadratic Gaussian Control Gravitational Effects Flexible Spacecraft Spacecraft Control Equations of Motion Linear Quadratic Regulator Large Space Structures Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |