The concept and philosophy for the organization of an RPV Flying Qualities Design Criteria are presented in a preliminary framework of criteria with supporting background and rationale. This report completes Phase II of a four-phase AFFDL/FGC program for the development of an RPV Flying Qualities Specification. The performance-oriented criteria are developed in hierarchical fashion from mission requirements, through total system requirements, to subsystem requirements. The criteria encompass automatic and manual controls, command and data link, controls and displays as well as vehicle stability and control. The material was based on an RPV literature search and review, and an evaluation of existing military specifications for piloted aircraft, such as MIL-F-8785B, MIL-F-83300, MIL-F-9490D (USAF), and MIL-C-18244A (Navy). (Author)
RPV Flying Qualities Design Criteria
1976
214 pages
Report
No indication
English
Aircraft , Aeronautics , Avionics , Remotely piloted vehicles , Flight control systems , Remote control , Flight maneuvers , Automatic , Manual operation , Missions , Specifications , Military requirements , Literature surveys , Data links , Man machine systems , Display systems , Guidance , Aerodynamic stability , Flight envelope , Handling , Aerodynamic characteristics , Design , Flying qualities
RPV flying qualities design criteria
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