06.2 - Flight Dynamics and Control (UAV related)
SIMULATION MODEL CALIBRATION USING SYSTEM IDENTIFICATION FOR A VECTORED-THRUST MULTI-TILT-ROTOR CONFIGURATION
B. Kunwar¹, S. Putra¹, R. Bhandari¹, C. McCormick¹, I. Chakraborty¹; ¹Auburn University, United States
This paper presents a simulation model development and calibration approach for a novel subscale aircraft configuration. A component-based aero-propulsive performance model, an actuator model, and experimental mass properties are incorporated into the MADCASP framework. The initial simulation model is then calibrated using data from system identification flight tests.
DOI: 10.71945/icas2026_0929