United States Department of Transportation
i
Simulation Model for the Convair CV-880 and Boeing 720 B Aircraft-Autopilot Systems in the Approach Configuration
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1971-07-01
[PDF-2.01 MB]
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Abstract:This report presents the basic equations and data required to simulate the Convair CV-880 and Boeing 720 B aircraft-autopilot systems in the approach configuration from altitude and heading hold down to flare. The approach maneuver is discussed in Section I. A fixed pilot aircraft model is assumed and is presented in Section II. It consists of linearized, rigid body, six-degree-of-freedom perturbation equations, trajectory equations and hinge moment equations.
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Content Notes:Introduction, Section 1: The approach maneuver, Section 2: Analytical model of aircraft, Section 3: Convair CV-880 aircraft data, Section 4: Boeing 720-B aircraft data, References
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