In this lesson we implemented aircraft glide path control, involving airspeed, glide slope, and pitch angle control loops are applied to the longitudinal dynamics of an aircraft to enable commanded tracking of glide slope and airspeed. We derive the appropriate models for control and establish the control architectures. The multi-loop system is tuned systematically with root locus and step responses. The full glide path control system is simulated and retuned to avoid throttle saturation. The resulting control system provides reasonable glide path tracking response for the transport aircraft. This system will be combined with flare path control and evaluated in nonlinear simulation.
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