Stability Result for Dynamic Inversion Devised to Control Large Flexible Aircraft

Topics:
Aerospace and Defense
Tags:
Aerospace & Defense,
Aircraft,
Manufacturing
Source:
NASA

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Overview: This paper is an initial attempt to establish global stability results for dynamic inversion methodology as applied to a large, flexible aircraft. This work builds on a previous result for rigid fighter aircraft and adds a new level of complexity that is the flexible aircraft dynamics, which cannot be ignored even in the most basic flight control. The results arise from observations of the control laws designed for a new generation of the High-Speed Civil Transport aircraft.

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Format: PDF | Size: 389KB | Date: Oct 2001 | Pages: 13

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