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- W858990038 abstract "An advanced structure for automatic flight control logic for powered-lift aircraft operating in terminal areas is under investigation at Ames Research Center. This structure is based on acceleration control; acceleration commands are constructed as the sum of acceleration on the reference trajectory and a corrective feedback acceleration to regulate path tracking errors. The central element of the structure, termed a Trimmap, uses a model of the aircraft aerodynamic and engine forces to calculate the control settings required to generate the acceleration commands. This report describes the design criteria for the Trimmap and derives a Trimmap for Ames experimental augmentor wing jet STOL research aircraft." @default.
- W858990038 created "2016-06-24" @default.
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- W858990038 date "1979-03-01" @default.
- W858990038 modified "2023-09-23" @default.
- W858990038 title "Configuration management and automatic control of an augmentor wing aircraft with vectored thrust" @default.
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