2022
DOI: 10.3390/rs14020402
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An In-Orbit Stereo Navigation Camera Self-Calibration Method for Planetary Rovers with Multiple Constraints

Abstract: In order to complete the high-precision calibration of the planetary rover navigation camera using limited initial data in-orbit, we proposed a joint adjustment model with additional multiple constraints. Specifically, a base model was first established based on the bundle adjustment model, second-order radial and tangential distortion parameters. Then, combining the constraints of collinearity, coplanarity, known distance and relative pose invariance, a joint adjustment model was constructed to realize the in… Show more

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Cited by 5 publications
(4 citation statements)
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“…This is essentially an implementation of a CAVHOR sensor model [42]. CAVHOR has been widely used in NASA's Mars rover missions and is described in Xu et al [43].…”
Section: Csm For Planetary Sensorsmentioning
confidence: 99%
“…This is essentially an implementation of a CAVHOR sensor model [42]. CAVHOR has been widely used in NASA's Mars rover missions and is described in Xu et al [43].…”
Section: Csm For Planetary Sensorsmentioning
confidence: 99%
“…After the Yutu-2 lunar rover is launched and operating in orbit, the internal and external parameters of the camera calibrated on the ground may change. Therefore, to improve the accuracy of subsequent lunar terrain constructions, the present study employs the in-orbit self-calibration method of stereo cameras with additional multiple constraints [27] to accurately determine the internal and external parameters of the cameras. After a navigation camera captures a surround image, its field of view contains its solar panels (as shown in Figure 3).…”
Section: Yutu-2 Navigation Camera Calibrationmentioning
confidence: 99%
“…where V 1 and V 2 are the image point residual corrections; V 3 is the correction of the 3D coordinates of the solar panel features; t 1 = [∆X l S , ∆Y l S , ∆Z l S , ∆φ l , ∆ω l , ∆κ l ] T and t 2 = [∆X r S , ∆Y r S , ∆Z r S , ∆φ r , ∆ω r , ∆κ r ] T are the corrections of the orientation elements inside the left and right images, respectively; X 1 = [∆x l 0 , ∆y l 0 , ∆ f l ] T and X 2 = [∆x r 0 , ∆y r 0 , ∆ f r ] T are the corrections of the inner orientation elements of the left and right images, respectively; X 3 = [∆X, ∆Y, ∆Z] T is the correction of the 3D coordinates of the solar panel features ; A, B, C, D, G, and F are the corresponding coefficient matrices; L l , L r , and L 3 are the residual matrices; P is the weight matrix corresponding to the observed quantity; and E is the identity matrix. Specific expressions for these parameters are provided in reference [27]. The least squares adjustment is applied to Equation (1) to obtain the substitution parameters (𝒕 𝟏 , 𝒕 𝟐 , 𝑿 𝟏 , and 𝑿 𝟐 ); the error in the unit weight is 0.210 pixels.…”
Section: Yutu-2 Navigation Camera Calibrationmentioning
confidence: 99%
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