Accession Number : AD1034465


Title :   Attitude Determination and Control System Design for a 6U Cube Sat for Proximity Operations and Rendezvous


Descriptive Note : Conference Paper


Corporate Author : Air Force Institute of Technology Wright-Patterson AFB United States


Personal Author(s) : Franquiz,Francisco J ; Edwards,Peter ; Udrea,Bogdan ; Nayak,Michael V ; Pueschl,Thorsten


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/1034465.pdf


Report Date : 04 Aug 2014


Pagination or Media Count : 19


Abstract : The work presented in this paper focuses on the design of an attitude determination and control subsystem (ADCS) for a proximity operation and imaging satellite mission. The ARAPAIMA (Application for Resident Space Object Proximity Analysis and IMAging) mission is carried out by a 6 U CubeSat class satellite equipped with a warm gas propulsion system. The propulsion system comprises an orbital maneuvering thruster which produces 100 mN and a set of 16 reaction control system (RCS) thrusters, of 25 mN each, installed in pairs that generate torques about each of the satellite body axes. The thrust of the RCS thrusters can be modulated over the entire range in steps of 1% due to the rapid solenoid valve actuation. The requirement of the control system is to provide pointing control accuracy of 1 arc min at 3 in the desired imaging direction. The ADCS employs two control aws. One control law, for large angle maneuvers, implements eigen axis maneuvering and the other, for accurate pointing, is implemented with PID controllers about each body axis.


Descriptors :   satellite attitude control , artificial satellites , determinants(mathematics) , air force , situational awareness , laser rangefinding , nanosatellites , maneuvers , propulsion systems , momentum , spacecraft


Subject Categories : Unmanned Spacecraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE