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A comparison of three random number generators for aircraft dynamic modeling applications
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Analogy between the Collatz Conjecture and sliding mode control
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Dependence of dynamic modeling accuracy on sensor measurements, mass properties, and aircraft geometry
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Dynamic modeling using output-error parameter estimation based on frequency responses estimated with multisine inputs
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In-flight turbulence emulation for fixed-wing aircraft using equivalent multisine excitations
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Output measurement equations for flexible aircraft flight dynamics
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Position corrections for airspeed and flow angle measurements on fixed-wing aircraft
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