KUMAR, N. S. Input Excitation Techniques for Aerodynamic Derivatives Estimation of Highly Augmented Fighter Aircraft. Defence Science Journal, [S. l.], v. 49, n. 3, p. 187–196, 2013. DOI: 10.14429/dsj.49.3828. Disponível em: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/3828. Acesso em: 17 aug. 2025.