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ＧＰＳ定姿线性化算法需要载体的姿态初值和迭代运算，提出一种适用于基线平面布局的矩阵元素求解算法，它不需初值和迭代计算，计算量小，运算速度快，特别适用于载体大角度姿态机动的情形。用ＴＡＮＳＶｅｃｔｏｒＧＰＳ接收机进行了实验，取得了较满意的结果。
The GPS attitude determination linearization algorithm needs the attitude initial value and iterative computation of the carrier, and proposes a matrix element solving algorithm suitable for the baseline plane layout, which requires no initial value and iterative computation, has a small amount of calculation and is fast in computation speed, and is particularly suitable for Vector large angle attitude maneuvering situation. Experiments with TANSVector GPS receiver have achieved satisfactory results.