Research Article

Attitude Determination Method by Fusing Single Antenna GPS and Low Cost MEMS Sensors Using Intelligent Kalman Filter Algorithm

Table 3

The STD in IKF and EKF.

STDRollPitchYaw
EKFIKFEKFIKFEKFIKF

Sec. 10.5564940.5266920.6449480.3354931.3170890.48039
Sec. 21.2512280.3773510.7824640.5466621.0785040.283883
Sec. 30.4695540.1764530.5807410.1163730.7234930.649624
Total0.65020.30350.71710.33471.49321.1556