METHOD AND DEVICE FOR POSITION CONTROL OF A SPACECRAFT
作者： Schateikis Tobias , Herdrich Georg , Fasoulas Stefanos
DOI:
关键词:
摘要: The invention relates to a method and device for position control of spacecraft (1). In the method, force is exerted on (1) by emitting at least one directed beam (7) electromagnetic radiation having sufficient power control, leading change in and/or orientation space. generated or more light-emitting diodes (8) arranged (1), effects said from Precise can be achieved controlling emission direction power. enable fuel-free with maximum precision.
lens.org 参考文章(6)
Louis A Ule, System for detecting and utilizing the maximum available power from solar cells ,(1970)
Young K. Bae, Photonic Laser Propulsion: Proof-of-Concept Demonstration Journal of Spacecraft and Rockets. ,vol. 45, pp. 153- 155 ,(2008) , 10.2514/1.32284
K. Iwami, Taku Akazawa, Tomohiro Ohtsuka, Hiroyuki Nishida, Norihiro Umeda, Nanonewton thrust measurement of photon pressure propulsion using semiconductor laser Proceedings of SPIE. ,vol. 8164, pp. 816406- ,(2011) , 10.1117/12.893427
Robert J Schwinghamer, Space vehicle electrical system ,(1962)
Mang Volker, Weber Karl-Heinz, Zier Manfred, Satellite position and path regulation method uses reflection of electromagnetic radiation by adjustable reflection surface mounted on satellite for providing correction drive pulse ,(2000)