Title:
VISORS Mission Orbit & Dynamics
Simulation Using a Realtime Dynamics
Processor
VISORS Mission Orbit & Dynamics
Simulation Using a Realtime Dynamics
Processor
Author(s)
Kimmel, Elizabeth
Advisor(s)
Lightsey, E. Glenn
Editor(s)
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Abstract
VIrtual Super-resolution Optics using Reconfigurable Swarms (VISORS) is a precision
formation-flying mission which uses two 6U CubeSats with a Science Mode separation
distance of 40 meters to emulate a 40-meter focal length diffractive optic telescope. Due to the
novelty of the technology used to achieve the stringent relative positioning requirements, the
dynamics of these orbits must be simulated to verify the concept of operations (ConOps), the
commercial spacecraft bus flight software (FSW), the guidance, navigation, and control
(GNC) formation-keeping algorithm, and the attitude determination and control system
(ADCS) performance, among others. Verifying these aspects helps ensure that issues such as
reaction wheel saturation, pointing errors, or collision risks, among others, do not arise during
the mission. This paper describes the work done in simulating the spacecraft dynamics during
the mission’s Science Operations using COSMOS to interface with the Realtime Dynamics
Processor (RDP) and spacecraft bus Engineering Design Unit (EDU) provided by Blue Canyon
Technologies (BCT).
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Date Issued
2023-12-01
Extent
Resource Type
Text
Resource Subtype
Masters Project
Rights Statement
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