Flight Control Research at NASA Ames

Hashemi, Kelley

关键词: AERODYNAMIC DRAG;    AEROELASTICITY;    AEROSERVOELASTICITY;    DYNAMIC CONTROL;    FLEXIBLE WINGS;    FLIGHT CONTROL;    GUST LOADS;    REAL TIME OPERATION;    TRANSONIC WIND TUNNELS;    WIND TUNNEL TESTS;   

RP-ID  :  ARC-E-DAA-TN67091

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

An overview of the flight control work in the Intelligent Systems Division at NASA Ames is presented. The highlight focuses on efforts surrounding performance-adaptive aeroelastic wing shaping for aircraft with flexible wings. Topics covered include aeroservoelastic modeling capabilities, online drag-optimizing control designs, gust and maneuver load alleviation techniques, and related wind tunnel demonstrations.