Navigation Solution Concept and Its Practical Approach Development for Lunar Missions

被引:2
作者
Akimov E.V. [1 ]
Kozorez D.A. [1 ]
Kruzhkov D.M. [1 ]
机构
[1] Moscow Aviation Institute, Moscow
关键词
lunar missions; navigation; radio navigation systems;
D O I
10.3103/S1068798X20070035
中图分类号
学科分类号
摘要
Abstract: Possible approaches to the creation of navigation systems for lunar missions are considered. Radio navigation systems of moderate wavelength are proposed, with a query model of data transmission using a network of stations. A model of the measurements taking account of the Nonius principle is considered. For a system with fixed initial characteristics, that improves the navigational precision without the need for any hardware or software modifications. The operational principle of the proposed navigation system is outlined, and its characteristics are assessed. © 2020, Allerton Press, Inc.
引用
收藏
页码:605 / 607
页数:2
相关论文
共 7 条
[1]  
(2019)
[2]  
(1968)
[3]  
Ivanyukhin A.V., Petukhov V.G., Low-energy sub-optimal low-thrust trajectories to libration points and halo-orbits, Cosm. Res, 57, pp. 378-388, (2019)
[4]  
Artuso G., Colonna Walewski A., Dragoniet M., Et al., Lunar navigation and positioning system based on cubesat constellation, Proc. 69Th Int. Astronautical Congr. “IAC 2018: Involving Everyone, (2018)
[5]  
Bagrov A.V., Dmitriev A.O., Leonov V.A., Et al., Global optical navigation system of the Moon, Tr. Mosk. Aviats. Inst., 99, (2018)
[6]  
LORAN.
[7]  
Ko S., Aikawa G., Takayama J., Ohyama S., A high-precision RF time-of-flight measurement method based on Vernier effect for localization of wireless sensor networks, Sens. Transducers J., 135, pp. 27-41, (2011)