Estimation and Analysis of Powered Phase’s Orbit of the Spacecraft Based on Multiple-Point Intersection Algorithm

Table 2

Position and velocity residuals of the two models.

	Position residuals (m)	Velocity residuals (m/s)
Model 1	4.09361e + 04	8.46286e + 02
Model 2	2.67343e + 04	6.39409e + 02