C-141 ALL WEATHER LANDING SYSTEM ENGINEERING SUPPORT
The systems and equipment described augment the capability of the standard C-141 Category II All Weather Landing System (AWLS) to operate in Category III weather conditions. This final report describes the physical location, operation, and theory of operation of the individual systems. A description of the on-board test instrumentation used to document the results of the AWLS test flights is included. A simulation model of the NC-141A test aircraft was developed to facilitate analysis of an AWLS operation on a system mock-up. The aircraft equations of motion which were used and the results of the simulation model testing are a part of this report.
- Sponsored in part by Federal Aviation Administration, Washington, D.C. Systems Research Development Service.
Lear Siegler, IncorporatedManagement Services Division, Wright-Patterson AFB
Dayton, OH United States 45433
- Kozina, J S
- Publication Date: 1976-6
- Pagination: 153 p.
- TRT Terms: Airborne navigational aids; All weather landing systems; Approach control; Automatic pilot (Aircraft); Cargo aircraft; Instrument flying; Landing; Landing aids; Radar
- Old TRIS Terms: Aircraft landings; All weather aviation; Approach indicators; Flight instruments
- Subject Areas: Aviation; Operations and Traffic Management;
- Accession Number: 00143254
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: Final Rpt., AFFDL-TR-76-46
- Contract Numbers: F33615-72-C-1358
- Files: NTIS, TRIS
- Created Date: Nov 3 1976 12:00AM