Читать книгу Global Navigation Satellite Systems, Inertial Navigation, and Integration - Mohinder S. Grewal - Страница 61

2.3.2.2 Navigation Solution Procedure

Оглавление

Transmitter positions x1, y1, x2, y2 are known; the transmitter locations are typically provided by the GNSS satellites or known to be at a fixed surveyed location for a terrestrial source. Signal travel times ΔT1, ΔT2 are measured by the system. Initially, the user positions are assumed. Set position coordinates X, Y equal to their initial estimates:


Compute the range errors:

(2.15)

(2.16)

Compute the θ angle (see Figure 2.3):

(2.17)

Compute update to user position:

(2.18)

(2.19)

Compute a new estimate of position using the update:

(2.20)

Continue to compute θ, ΔR1, and ΔR2 from these equations with new values of . Iterate Eqs. (2.15)(2.20) and stop when Δx and Δy become less than the desired accuracy:


Global Navigation Satellite Systems, Inertial Navigation, and Integration

Подняться наверх