AIAA Guidance, Navigation, and Control Conference 2012
DOI: 10.2514/6.2012-4701
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Visual-Inertial Estimation and Control for Inspection of a Tumbling Spacecraft: Experimental Results from the International Space Station

Abstract: Large spacecraft represent a large investment of time and money, and are often risky ventures. The ability to visually inspect craft provides operators and engineers valuable information about on-orbit failures or salvagability. To minimize the risk of damage to the large craft, initial inspection maneuvers should be designed to maintain a safe observation distance. This paper discusses the design of such an inspection maneuver using range measurements that are directly applicable to stereo vision and are supp… Show more

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Cited by 4 publications
(1 citation statement)
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“…In addition, the effects of disturbance torques acting on the target are modeled as zero-mean Gaussian noises added on the angular acceleration with covariance E{𝜺𝜺 T } = 0.1 2 I 3×3 (N⋅m) 2 . 26 It is initially assumed that the quaternion-expression attitude measurements of the space debris are provided by noncontact measure methods, denoted by {z k }. The measurement errors are also assumed zero-mean Gaussian noises with covariance R k = E{z k z T k } = 0.05 2 I 4×4 .…”
Section: Simulation Studiesmentioning
confidence: 99%
“…In addition, the effects of disturbance torques acting on the target are modeled as zero-mean Gaussian noises added on the angular acceleration with covariance E{𝜺𝜺 T } = 0.1 2 I 3×3 (N⋅m) 2 . 26 It is initially assumed that the quaternion-expression attitude measurements of the space debris are provided by noncontact measure methods, denoted by {z k }. The measurement errors are also assumed zero-mean Gaussian noises with covariance R k = E{z k z T k } = 0.05 2 I 4×4 .…”
Section: Simulation Studiesmentioning
confidence: 99%