Evaluation of Matrix Square Root Operations for UKF within a UAV GPS/INS Sensor Fusion Application

Table 4

Summary of the distribution of flight conditions.

Approximate flight condition	Minimum	Maximum	Mean	Standard deviation
Temperature (°F)	38	86	65.1	13.9
Wind speed (mph)	0	11	5.8	3.5
Flight duration (sec)	375	640	485	76.0