“…However, in these methods, a long alignment time (more than 300 seconds) is required to ensure sufficient random noise smoothing and time intervals between two vectors to avoid collinearity and ensure solution accuracy with the dual‐vector method. The second method is attitude‐optimization‐based initial alignment, which transforms the initial alignment problem into a continuous attitude determination problem by using infinite vector observations (Ben et al., 2011; Chang, Li, & Chen, 2015; Kang, Fang, & Wang, 2013; Kang, Ye, & Song, 2014; Li, Tang, Lu, & Wu, 2013; Wu & Pan, 2013; Wu, Wu, Hu, & Hu, 2011; Zhou, Qin, Zhang, & Cheng, 2012). All these methods listed in these papers are based on the decomposition of the attitude matrix into earth motion, inertial rate, and alignment matrix, but have different vector observation constructions and alignment matrix calculation procedures.…”