Performance Analysis of Apollo Navigational Starter Routine (1905)
Ivanov, Stoyan I., Holt, Gre · leaf 11
;B 5„ - X Component - Y Component - Z Component - Diflerence Magnitude Figure 3: The Return Trajectory critical point for Range and Angle noise is the same as thatfor Earth Orbit. Above Noise Level 20RA, the state vector estimation begins to greatlydiverge from the truth, the plot shows this as an… … Figure 4: The Retum Trajectory critical point for Range and Angle noise is supported bythe RMS plot. After the same critical point, 20RA noise, the RMS begins to rapidly climb,and the confidence in the solution deteriorates proportionally. 12 Lunar Orbit Magnitude of Difference Between Converged…
