Systems Engineering and Electronics ›› 2026, Vol. 48 ›› Issue (4): 1370-1377.doi: 10.12305/j.issn.1001-506X.2026.04.25
• Guidance, Navigation and Control • Previous Articles
Zhongzhong ZHENG1, Jie GUO1,*, Yangyang WAN1, Yulin WANG2, Shengjing TANG1
Received:2025-03-25
Revised:2025-05-06
Online:2025-12-08
Published:2025-12-08
Contact:
Jie GUO
CLC Number:
Zhongzhong ZHENG, Jie GUO, Yangyang WAN, Yulin WANG, Shengjing TANG. Survey of SO(3)-based spacecraft attitude error description methods[J]. Systems Engineering and Electronics, 2026, 48(4): 1370-1377.
Table 1
Characteristics of attitude description methods for spacecraft"
| 姿态描述方法 | 优势 | 不足 |
| SO(3) | 无奇异,能全局描述姿态,无超越函数运算,可用于连续旋转 | 6个冗余,不直观,计算量大,数学意义复杂,传感器无法直接获取 |
| 欧拉角 | 无冗余参数,物理意义明确,传感器获取方便 | 在 |
| 罗格里斯参数 | 无冗余,较少的超越函数运算,可用于连续旋转 | 在 |
| 修正罗格里斯参数 | 无冗余,较少的超越函数运算,可用于连续旋转 | 在 |
| 四元数 | 无奇异,无超越函数运算,可用于连续旋转表示 | 在 |
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