Loading...
Please wait, while we are loading the content...
Similar Documents
Lockheed l-1101 avionic flight control redundant systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Throndsen, E. O. |
| Copyright Year | 1976 |
| Description | The Lockheed L-1011 automatic flight control systems - yaw stability augmentation and automatic landing - are described in terms of their redundancies. The reliability objectives for these systems are discussed and related to in-service experience. In general, the availability of the stability augmentation system is higher than the original design requirement, but is commensurate with early estimates. The in-service experience with automatic landing is not sufficient to provide verification of Category 3 automatic landing system estimated availability. |
| File Size | 1204373 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760024080 |
| Archival Resource Key | ark:/13960/t42r8mj2q |
| Language | English |
| Publisher Date | 1976-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Component Reliability Aircraft Stability Redundancy Automatic Flight Control Reliability Engineering Automatic Landing Control Avionics Yaw Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
