Polarization Navigation Simulation System and Skylight Compass Method Design Based upon Moment of Inertia

Figure 7

Procedure of the simulation. (a) DOP of the Rayleigh sky model; (b) AOP of the Rayleigh sky model; (c) hypothetical DOP image; (d) hypothetical AOPLM image; (e) the result of orientation determination shown on the hypothetical DOP image; (f) the result of orientation determination shown on the hypothetical AOPLM image. The yellow point represents the Sun and the white dotted line represents the result of orientation determination.