APA (7th ed.) Citation

Zhang, G., Chen, X., Xi, R., & Li, H. Nonsingular Integral Sliding Mode Attitude Control for Rigid-Flexible Coupled Spacecraft with High-Inertia Rotating Appendages. Wiley.

Chicago Style (17th ed.) Citation

Zhang, Gaowang, Xueqin Chen, Ruichen Xi, and Huayi Li. Nonsingular Integral Sliding Mode Attitude Control for Rigid-Flexible Coupled Spacecraft with High-Inertia Rotating Appendages. Wiley.

MLA (9th ed.) Citation

Zhang, Gaowang, et al. Nonsingular Integral Sliding Mode Attitude Control for Rigid-Flexible Coupled Spacecraft with High-Inertia Rotating Appendages. Wiley.