[1] Xuan M. Analysis of Chinas nano and microsatellite industry development［J］. Aerospace China, 2019, 20(1): 40-46.

[3] Poghosyan A, Golkar A. CubeSat evolution: Analyzing CubeSatcapabilities for conducting science missions［J］. Progress in Aerospace Sciences, 2016, 88(1): 59-83.

[4] Pelemeshko A, Kolesnikova A, Melkov A, et al. High-precision CubeSat sun sensor coupled with infrared earth horizon detector［J］. IOP Conf. Series: Materials Science and Engineering, 2020, 734: 012012.

[6] Zhang H, Niu Y X, Lu J Z, et al. Accurate and autonomous star acquisition method for star sensor under complex conditions［J］. Mathematical Problems in Engineering, 2017, 2017: 1-12.

[7] Kim S J, Kim S O, Moon B Y, et al. Development of ultra-light 2-axes sun sensor for small satellite［J］. J. of Astronomy & Space Sciences, 2005, 22(6): 47-58.

[8] Boom K, Leijtens J. Mini and micro sensor systems: Where small does not mean immature［C］// AIAA Guidance, Navigation and Control Conf. and Exhibit. 2008.

[9] Delgado F J, Quero J M, Garcia J, et al. Accurate and wide-field-of-view MEMS-based sun sensor for industrial applications［J］. IEEE Trans. on Industrial Electronics, 2012, 59(12): 4871-4880.

[11] Xie N, Theuwissen A J P. An autonomous micro digital sun sensor by a CMOS imager in space application［J］. IEEE Trans. on Electron Devices, 2012, 59(12): 3405-3410.

[13] Liebe C C, Murphy N, Dorsky L, et al. Three-axis sun sensor for attitude determination［J］. IEEE Aerospace and Electronic Systems Magazine, 2016, 31(6): 6-11.