Trimming and Linearization of the HL-20 Airframe
This is Part 1 of a five-part example series on design and tuning of the flight control
system for the HL-20 vehicle. This part deals with trimming and linearization of the
airframe.
HL-20 Model
The HL-20 model is adapted from the model described in “NASA HL-20 Lifting Body
Airframe” (Aerospace Blockset). This is a 6-DOF model of the vehicle during the final
descent and landing phase of the flight. No thrust is used during this phase and the
airframe is gliding to the landing strip.
open_system('csthl20_trim')
11 Gain-Scheduled Controllers