Ren, Y., & Xing, A. Finite-time attitude tracking control for spacecraft based on backstepping method with input saturation. Public Library of Science (PLoS).
Chicago Style (17th ed.) CitationRen, Yanmin, and Aijia Xing. Finite-time Attitude Tracking Control for Spacecraft Based on Backstepping Method with Input Saturation. Public Library of Science (PLoS).
MLA (9th ed.) CitationRen, Yanmin, and Aijia Xing. Finite-time Attitude Tracking Control for Spacecraft Based on Backstepping Method with Input Saturation. Public Library of Science (PLoS).
Warning: These citations may not always be 100% accurate.