Set-oriented design of interplanetary low-thrust trajectories using Earth Gravity Assist

2019 ◽  
Vol 156 ◽  
pp. 208-218 ◽  
Author(s):  
Daisuke Tamakoshi ◽  
Hirohisa Kojima
2006 ◽  
Vol 43 (1) ◽  
pp. 121-129 ◽  
Author(s):  
Byoungsam Woo ◽  
Victoria L. Coverstone ◽  
Michael Cupples

2009 ◽  
Vol 32 (2) ◽  
pp. 616-625 ◽  
Author(s):  
Ian Carnelli ◽  
Bernd Dachwald ◽  
Massimiliano Vasile

2011 ◽  
Vol 54 (4) ◽  
pp. 756-769 ◽  
Author(s):  
TieDing Guo ◽  
FangHua Jiang ◽  
HeXi Baoyin ◽  
JunFeng LI

1999 ◽  
Vol 22 (5) ◽  
pp. 637-642 ◽  
Author(s):  
Lorenzo Casalino ◽  
Guido Colasurdo ◽  
Dario Pastrone

2019 ◽  
Vol 11 (22) ◽  
pp. 2717 ◽  
Author(s):  
David Doelling ◽  
Konstantin Khlopenkov ◽  
Conor Haney ◽  
Rajendra Bhatt ◽  
Brent Bos ◽  
...  

The Earth-viewed images acquired by the space probe OSIRIS-REx during its Earth gravity assist flyby maneuver on 22 September 2017 provided an opportunity to radiometrically calibrate the onboard NavCam imagers. Spatially-, temporally-, and angularly-matched radiances from the Earth viewing GOES-15 and DSCOVR-EPIC imagers were used as references for deriving the calibration gain of the NavCam sensors. An optimized all-sky tropical ocean ray-matching (ATO-RM) calibration approach that accounts for the spectral band differences, navigation errors, and angular geometry differences between NavCam and the reference imagers is formulated in this paper. Prior to ray-matching, the GOES-15 and EPIC pixel level radiances were mapped into the NavCam field of view. The NavCam 1 ATO-RM gain is found to be 9.874 × 10−2 Wm−2sr−1µm−1DN−1 with an uncertainty of 3.7%. The ATO-RM approach predicted an offset of 164, which is close to the true space DN of 170. The pre-launch NavCam 1 and 2 gains were compared with the ATO-RM gain and were found to be within 2.1% and 2.8%, respectively, suggesting that sensor performance is stable in space. The ATO-RM calibration was found to be consistent within 3.9% over a factor of ±2 NavCam 2 exposure times. This approach can easily be adapted to inter-calibrate other space probe cameras given the current constellation of geostationary imagers.


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