Aircraft Aerodynamics and Pitch Control MapleSim Model - Aircraft Aerodynamics and Pitch Control S-Function - MapleSim Model Gallery

Aircraft Aerodynamics and Pitch Control

This model simulates the aerodynamics of an aircraft, incorporating the aircraft body model, aerodynamic data, and controller design. The aircraft body is characterized through a mass and inertia matrix, and driven through applied forces to the rigid body centre of mass frame. Nonlinear functions of angle-of-attack, air density variations, and more are implemented with lookup table data.

The attached OptimalControl and ControlLQG templates provide analysis and optimizations for controller design.

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Model Images
  • AircraftAerodynamics Custom CAD geometry helps to illustrate the aircraft aerodynamics seen here.
  • model Model diagram of aircraft body, aerodynamic data, and controller design.
  • plots Output of altitude and angle of attack.
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