Identification of aircraft longitudinal aerodynamic parameters using an online corrective test for wind tunnel virtual flight

• Published in: Chinese journal of aeronautics Vol. 37; no. 9; pp. 261 - 275
• Main Authors: TAI, Shang, BU, Chen, WANG, Yanling, YUE, Ting, LIU, Hailiang, WANG, Lixin
• Format: Journal Article
• Language: English
• Published: Elsevier Ltd 01.09.2024; School of Aeronautical Science and Engineering,Beihang University,Beijing 100191,China%AVIC Aerodynamics Research Institute,Harbin 150001,China
• Subjects: Aerodynamic parameter identification; Displacement constraints; Flight control law; Online solution; Wind tunnels; Aerodynamic parameter identification; Displacement constraints; Online solution; Wind tunnels; Flight control law

The identification of aerodynamic parameters is accomplished through the test data of the dynamic movement of scaled aircraft models flying dynamically in wind tunnel, which can realize the accurate acquisition of the aerodynamic model of the aircraft in the preliminary stage for aircraft design, an...