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Mcc level c formulation requirements. shuttle taem guidance and flight control, sts-1 baseline
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carman, G. L. Montez, M. N. |
| Copyright Year | 1980 |
| Description | The TAEM guidance and body rotational dynamics models required for the MCC simulation of the TAEM mission phase are defined. This simulation begins at the end of the entry phase and terminates at TAEM autoland interface. The logic presented is the required configuration for the first shuttle orbital flight (STS-1). The TAEM guidance is simulated in detail. The rotational dynamics simulation is a simplified model that assumes that the commanded rotational rates can be achieved in the integration interval. Thus, the rotational dynamics simulation is essentially a simulation of the autopilot commanded rates and integration of these rates to determine orbiter attitude. The rotational dynamics simulation also includes a simulation of the speedbrake deflection. The body flap and elevon deflections are computed in the orbiter aerodynamic simulation. |
| File Size | 2120386 |
| Page Count | 84 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800019907 |
| Archival Resource Key | ark:/13960/t73v4cv30 |
| Language | English |
| Publisher Date | 1980-06-01 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Brakes for Arresting Motion Terminal Area Energy Management Guidance Motion Rotating Bodies Automatic Pilots Flight Control Space Shuttle Orbiters Computer Programs Ground Tracks Speed Control Roll Sequencing Space Transportation System 1 Flight 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 |
