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Altitude Hold Autopilot

Project type

Simulation

Date

August 2023

Location

Dallas, Texas

Role

Control Systems Engineer

Tools

MATLAB / Simulink

Control Method

Proportional Control

Focus Area

Aircraft Stability & Altitude Regulation

Designed and implemented an altitude hold autopilot system in Simulink using a state-space model of an aircraft. Angle of attack and pitch feedback were incorporated for stability augmentation, with proportional control applied to regulate altitude. The controller gain was tuned using pole placement in SISO Tool, meeting targeted criteria for steady-state time and percentage overshoot under nominal conditions.

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