Loading...
Please wait, while we are loading the content...
Similar Documents
Pinhole occulter experiment
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pflug, John Ring, Jeff |
| Copyright Year | 1987 |
| Description | Viewgraphs and charts from a briefing summarize the accomplishments, results, conclusions, and recommendations of a feasibility study using the Pinhole Occulter Facility (POF). Accomplishments for 1986 include: (1) improved IPS Gimbal Model; (2) improved Crew Motion Disturbance Model; (3) use of existing shuttle on-orbit simulation to study the effects of orbiter attitude deadband size on POF performance; (4) increased understanding of maximum performance expected from current actuator/sensor set; (5) use of TREETOPS nonlinear time domain program to obtain system dynamics describing the complex multibody flexible structures; (6) use of HONEY-X design tool to design and evaluate multivariable compensator for stability, robustness, and performance; (7) application of state-of-the-art compensator design methodology Linear Quadratic Gaussian/Loop Transfer Recovery (LQG/LTR); and (8) examination of tolerance required on knowledge of the POF boom flexible mode frequencies to insure stability, using structure uncertainty analysis. |
| File Size | 4522148 |
| Page Count | 141 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880002099 |
| Archival Resource Key | ark:/13960/t7pp40c27 |
| Language | English |
| Publisher Date | 1987-02-27 |
| Access Restriction | Open |
| Subject Keyword | Optics Controllers Gimbals Flexible Spacecraft Pinhole Occulter Facility Space Shuttle Orbiters Space Stations Compensators Spacecrews Systems Engineering Tolerances Mechanics Booms Equipment Mathematical Models Applications Programs Computers Spacecraft Stability Space Transportation System Computer Aided Design 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 | Technical Report |