A simplified guidance system for air-to-air missiles is described, where the pilot adjusts his helmet sight to compensate for missile errors and this information is fed to a computer which computes correction data from error information, aircraft position information and missile position information. Correction data is then sent via a radio link to the missile control system which changes the flight path accordingly. (Author)
Simplified High Accuracy Guidance System
1976
11 pages
Report
No indication
English
Simplified High Accuracy Guidance System
NTIS | 1976
|SIMPLIFIED MIDCOURSE GUIDANCE TECHNIQUES
AIAA | 1966
|Simplified midcourse guidance techniques.
NTRS | 1966
|