Fig. 1. Space satellite solar wing configuration. (a) Solar wing configuration^[17]; (b) coupling CPC solar wing space satellite structure

Fig. 2. Concentrating surface type physical structure. (a) S-CPC and intercepted S-CPC (in dashed box); (b) TMS-CPC

Fig. 3. Coupling TMS-CPC solar wing concentrating performance verification. (a) Solar wing TMS-CPC laser experiment; (b) simulation and experimental values of laser experiment

Fig. 4. Optical efficiency of solar wing TMS-CPC and S-CPC under different incident light

Fig. 5. Schematic diagrams of space orbit. (a) Relationship between eccentricity anomaly E and true anomaly v; (b) positional relationship among the sun, the earth, and the satellite

Fig. 6. Earth's shading effect on sun's rays

Fig. 7. Model verification of receiving of solar radiation by surface of solar wing of orbiting satellite

Fig. 8. Variation law of energy flux density distribution on the surface of solar wing with light incident angle

Fig. 9. Uniformity of energy flow on surface of battery panel in receiving half-angle

Fig. 10. Generated power of satellite solar wing. (a) Generated power of conventional satellite solar wing; (b) generated power of coupling CPC solar wing