Manoeuvre Controller Design for an F-111C Flight Dynamics Model

Abstract

A maneuver controller program has been developed to fly an F-111C dynamic flight model through any number of prescribed maneuvers. A selection of discrete maneuvers is available which can be used as building blocks to represent most of those likely to be encountered in flight. Generalized maneuvers can also be flown by providing reference flight trajectories generated by an external source. The dynamic model and maneuver controller have been developed to allow the realistic modeling of maneuvers required by mission analyses, weapons delivery studies and systems assessments.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 01, 1998
Accession Number
ADA352580

Entities

People

  • Peter W. Gibbens

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Control Surfaces
  • Aerodynamic Forces
  • Airborne Warning And Control System
  • Aircrafts
  • Airframes
  • Altitude Controllers
  • Control Sticks
  • Control Surfaces
  • Control Systems
  • Control Systems Engineering
  • Dynamic Response
  • Electrical Engineering
  • Horizontal Stabilizers
  • Information Systems
  • Mathematical Models
  • Military Aircraft
  • Navigation

Fields of Study

  • Physics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Computational Modeling and Simulation
  • Maritime Combat Support and Expeditionary Logistics.