Simulation Model for the Convair CV-880 and Boeing 720 B Aircraft-Autopilot Systems in the Approach Configuration

Details

• Creators:
  Koziol, J. S.
• Corporate Creators:
  John A. Volpe National Transportation Systems Center (U.S.)
• Subject/TRT Terms:
  • Simulation
  • Automatic pilot (Ships)
  • Flight control systems
  • Instrument landing systems
  • Mathematical models
  • Computer models
  • Automatic pilot
  • Flight control systems
  • Instrument landing systems
  • Simulation
  More +
• Publication/ Report Number:
  DOT-TSC-FAA-71-12
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Corporate Publisher:
  United States. Department of Transportation. Federal Aviation Administration
• 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.
• 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
• Format:
  PDF
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/9443/dot_9443_DS1.pdf
• File Type:
  [PDF - 2.01 MB]
• Collection(s):
  Volpe Center
• Main Document Checksum:
  urn:sha-512:88ca3f43f9c1c43a351487fc56d4a47c74ac5a49aa09236b7120d8cf4213a7b28dfb1341e9eceaf3d78e31ef835a217a472a8a4923b015dce1d51c915e2b8804