Close Proximity Spacecraft Operations Using Stereoscopic Imaging
The relative guidance, navigation, and control of a pair of spacecraft using real-time data from a stereoscopic imaging sensor are investigated. Because line-of-sight measurements from a single imager are typically insufficient for system observability, a second imager with a known baseline vector to the first imager is included to achieve system observability with the addition of relative range measurements. The stereoscopic imaging system as modeled provides measurements capable of achieving a complete navigation solution. An SDRE controller is used to provide closed-loop control to maintain a desired relative orbit. An Unscented Kalman Filter is used to estimate the chief spacecraft's inertial states using GPS measurements and the deputy spacecraft's inertial states with stereoscopic imaging relative position measurements. Relative Orbital Elements are implemented to model separation between the spacecraft. © 2013 2013 California Institute of Technology.
J. Darling et al., "Close Proximity Spacecraft Operations Using Stereoscopic Imaging," 23rd AAS/AIAA Space Flight Mechanics Meeting, Spaceflight Mechanics 2013, Univelt Inc., Jan 2013.
23rd AAS/AIAA Space Flight Mechanics Meeting, Spaceflight Mechanics 2013
Mechanical and Aerospace Engineering
Keywords and Phrases
Observability; Space Flight; Line-Of-Sight Measurements; Relative Orbital Elements; Relative Position Measurement; Spacecraft Operation; Stereoscopic Imaging; Stereoscopic Imaging System; System Observability; Unscented Kalman Filter
Article - Conference proceedings
© 2013 Univelt Inc., All rights reserved.
This document is currently not available here.