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Analyses of shuttle orbiter approach and landing conditions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hoh, R. H. Ashkenas, I. L. Dimarco, R. J. Teper, G. L. |
| Copyright Year | 1981 |
| Description | A study of one shuttle orbiter approach and landing conditions are summarized. Causes of observed PIO like flight deficiencies are identified and potential cures are examined. Closed loop pilot/vehicle analyses are described and path/attitude stability boundaries defined. The latter novel technique proved of great value in delineating and illustrating the basic causes of this multiloop pilot control problem. The analytical results are shown to be consistent with flight test and fixed base simulation. Conclusions are drawn relating to possible improvements of the shuttle orbiter/digital flight control system. |
| File Size | 8949448 |
| Page Count | 137 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810018575 |
| Archival Resource Key | ark:/13960/t7wm63q79 |
| Language | English |
| Publisher Date | 1981-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Flight Conditions Digital Systems Approach and Landing Tests Sts Transfer Functions Flight Control Aerodynamic Characteristics Space Shuttle Orbiters 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 |
