Precise attitude determination strategy for spacecraft based on information fusion of attitude sensors: Gyros/GPS/Star-sensor

MLA

Mao Xinyuan, et al. “Precise Attitude Determination Strategy for Spacecraft Based on Information Fusion of Attitude Sensors: Gyros/GPS/Star-Sensor.” International Journal of Aeronautical and Space Sciences, vol. 14, Mar. 2013, pp. 91–98. EBSCOhost, https://doi.org/10.5139/ijass.2013.14.1.91.

APA

Mao Xinyuan, Du Xiaojing, & Fang Hui. (2013). Precise attitude determination strategy for spacecraft based on information fusion of attitude sensors: Gyros/GPS/Star-sensor. International Journal of Aeronautical and Space Sciences, 14, 91–98. https://doi.org/10.5139/ijass.2013.14.1.91

Chicago

Mao Xinyuan, Du Xiaojing, and Fang Hui. 2013. “Precise Attitude Determination Strategy for Spacecraft Based on Information Fusion of Attitude Sensors: Gyros/GPS/Star-Sensor.” International Journal of Aeronautical and Space Sciences 14 (March): 91–98. doi:10.5139/ijass.2013.14.1.91.