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)


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    RPV flying qualities design criteria

    NEIGHBOR, T. / WILER, C. | AIAA | 1978




    Mission-specific flying qualities criteria

    Page, Mark / Gillette, Darrell | AIAA | 1994


    Mission-Specific Flying Qualities Criteria

    Page, M. / Gillette, D. / AIAA | British Library Conference Proceedings | 1994