Jinlong Z, Jianhong W, Ruchun W, Xi L, Yongjun D, Azar AT, et al. Control Design of the Quadrotor Aircraft based on the Integral Adaptive Improved Integral Backstepping Sliding Mode Scheme. Eng. Technol. Appl. Sci. Res. [Internet]. 2024 Oct. 9 [cited 2026 Jun. 3];14(5):17106-17. Available from: https://www.etasr.com/index.php/ETASR/article/view/8361