Overview and GNC design of the CubeSat Proximity Operations Demonstration (CPOD) mission

被引:37
|
作者
Roscoe, Christopher W. T. [1 ]
Westphal, Jason J. [1 ]
Mosleh, Ehson [2 ]
机构
[1] Appl Def Solut Inc, 10440 Little Patuxent Pkwy,Suite 600, Columbia, MD 21044 USA
[2] Tyvak Nanosatellite Syst Inc, 15265 Alton Pkwy,Suite 200, Irvine, CA 92618 USA
关键词
RELATIVE MOTION;
D O I
10.1016/j.actaastro.2018.03.033
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The CubeSat Proximity Operations Demonstration (CPOD) mission will demonstrate rendezvous, proximity operations, and docking with a pair of 3U CubeSats using miniaturized components and sensors. The goal of this mission is to develop small spacecraft technologies with game-changing potential and validate these technologies via spaceflight. Several new systems have been designed specifically for this program, including: next generation star trackers, next generation miniature reaction wheels, miniature cold-gas multi-thruster propulsion modules, a new relative navigation sensor suite, power management and distribution electronics based on flight proven designs, and intelligent software solutions hosted on multiple low-power Linux ARM processors. This paper will present an overview of the CPOD spacecraft and the mission Concept of Operations, as well as the design of the formation flying guidance, navigation, and control subsystem and algorithms.
引用
收藏
页码:410 / 421
页数:12
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