“…Set d 1 = 10 m, d 2 = 5 m, d x = 7 m, d y = 3 m, the error variance of the original baseline phase interferometer is σ ϕ = 0.0175 rad, and the measurement accuracy of the additional phase interferometer on fuselage axis and wing axis satisfies σ x ≤ 0.0776 rad and σ y ≤ 0.1567 rad, respectively –. For convenience, we choose σ x = 0.0776 rad and σ y = 0.1567 rad, the position of the fixed target is (107.15, 399.88, 0) km, the starting position of the observation platform is (0, 0, 10) km, the moving velocity of the observation platform is (300, 0, 0) m/s, the frequency of the target radiation signal is f T = 3 × 10 9 Hz, and signal observation interval is T = 1 second.…”