Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison With ... PDF
114 Pages·2000·2.98 MB·English
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Dryden Flight Research Facility. Edwards .. Figure 28. Pitch rate due to longitudinal stick AR—PA mode; M = 0.258, h = 4,000 ft. linear model that was used for the control law development. The X-29A .. For the normal digital modes the stick and rudder pedal input units are in percent of full thro
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