Analytical display design for flight tasks conducted under instrument meteorological conditions. [human factors engineering of pilot performance for display device design in instrument landing systems]
MetadataShow full item record
Paramount to proper utilization of electronic displays is a method for determining pilot-centered display requirements. Display design should be viewed fundamentally as a guidance and control problem which has interactions with the designer's knowledge of human psychomotor activity. From this standpoint, reliable analytical models of human pilots as information processors and controllers can provide valuable insight into the display design process. A relatively straightforward, nearly algorithmic procedure for deriving model-based, pilot-centered display requirements was developed and is presented. The optimal or control theoretic pilot model serves as the backbone of the design methodology, which is specifically directed toward the synthesis of head-down, electronic, cockpit display formats. Some novel applications of the optimal pilot model are discussed. An analytical design example is offered which defines a format for the electronic display to be used in a UH-1H helicopter in a landing approach task involving longitudinal and lateral degrees of freedom.
Approved for public release, distribution unlimited
Showing items related by title, author, creator and subject.
Designs for Large-Scale Simulation Experiments, with Applications to Defense and Homeland Security Sanchez, Susan M.; Lucas, Thomas W.; Sanchez, Paul J.; Nannini, Christopher J.; Wan, Hong (2012-02);Computer experimentation is integral to modern scientific research, national defense, industry and manufacturing, and in public policy debates. Traditional design of experiments (DOE) focuses on small-scale experimentation, ...
Gong, Qi; Ross, Michael I.; Alfriend, Terry (The American Institute of Aeronautics and Astronautics (AIAA), 2008-08-18);In this paper, we further a general framework for the formation design of distributed space systems. Based on constrained nonlinear optimal control theory, the formation of multi-spacecraft is designed by Pseudospectral ...
Agrawal, B.N. (2005);This paper presents a review of the spacecraft design program at the Naval Postgraduate School. This program is part of the space systems engineering curriculum. In this curriculum, the students take at least one course ...