Aircraft Guidance and Control System Synthesis for Approach and Landing Studies.
Final rept. 1 Aug 69-31 Dec 70,
LEAR SIEGLER INC OKLAHOMA CITY OK MANAGEMENT SERVICES DIV
Pagination or Media Count:
RD Systems were synthesized and evaluated in four T-39A aircraft. Flight control and display concepts were developed to optimize navigation and guidance requirements. Successful automatic approaches through flare and touchdown were routinely accomplished even under minimum weather conditions. Thus, the systems as synthesized provided a solution to the basic problem.
- Flight Control and Instrumentation