Requirement Analysis of Navigation System for Lunar Lander According to Mission Conditions |
Park, Young Bum
(Department of Mechanical and Aerospace Engineering, Seoul National University)
Park, Chan Gook (Department of Mechanical and Aerospace Engineering, Seoul National University) Kwon, Jae Wook (Korea Aerospace Research Institute) Rew, Dong Young (Korea Aerospace Research Institute) |
1 | Tye, B., Stephen, P., and Timothy, C., "GN&C Development for Future Lunar Landing Missions," AIAA Guidance, Navigation, and Control Conference. 2010. |
2 | Brady, T. and Schwartz, J., "ALHAT System Architecture and Operational Concept," IEEE Aerospace Conference, 2007. |
3 | DeMars, K. J. and Bishop, R. H., "Precision Descent Navigation for Landing at the Moon," Advances in the Astronautical Sciences, 129(2), 2008, pp. 1027-1050. |
4 | Geller, D.K. and Christensen, D., "Linear Covariance Analysis for Powered Lunar Descent and Landing," Journal of Spacecraft and Rockets, 46(6), 2009, pp. 1231-1248. DOI |
5 | Melloni, S., et al, "GNC Solutions for Next-Moon Lunar Lander Mission," 21th International Symposium on Space Flight Dynamics, 2009. |
6 | Ely, T. A., Heyne, M., and Riedel, J. E., "Altair Navigation During Translunar Cruise, Lunar Orbit, Descent, and Landing," Journal of Spacecraft and Rockets, 49(2), 2012, pp. 295-317. DOI |
7 | Ku, P. M., Park, Y. B., and Park, C. G., "Performance Analysis of Batch Process Terrain Relative Navigation Using Area based Terrain Roughness Index for Lunar Lander," Jouranl of The Society for Aeronautical and Space Sciences, 44(7), 2016, pp. 629-639. |
8 | Li, S., Jiang, X., and Tao, T., "Guidance Summary and Assessment of the Chang'e-3 Powered Descent and Landing," Journal of Spacecraft and Rockets, 53(2), 2016, pp. 258-277. DOI |
9 | Huxel, P. J. and Cohanim, B. E., "Small lunar lander/hopper navigation analysis using linear covariance," IEEE Aerospace Conference, 2010. |
10 | Gelb, A., Applied Optimal Estimation, MIT Press, Cambridge, MA, 1974. |
11 | Titterton, D. and Weston, J. L., Strapdown Inertial Navigation Technology, 2nd Edition, Reston, VA, American Institute of Aeronautics and Astronautics, 2004. |
12 | Robert, H.B., et al., "An Inertial Dual-State State Estimator for Precision Planetary Landing with Hazard Detection and Avoidance," AIAA Guidance, Navigation, and Control Conference, 2016. |
13 | Pittelkau, M. E., "Kalman Filtering for Spacecraft System Alignment Calibration," Journal of Guidance, Control, and Dynamics, 24(6), 2001, pp. 1187-1195. DOI |
14 | Zanetti, R., Advanced Navigation Algorithm for Precision Landing, PhD thesis, The University of Texas at Austin, 2007. |
15 | Trawny, N., et al., "Vision-aided inertial navigation for pin-point landing using observations of mapped landmarks," Journal of Field Robotics, 24(5), 2007, pp. 357-378. DOI |
16 | Roh, W. R., et al., "Development of Fiber Optic Gyro for KSLV-II Inertial Navigation Guidance Unit," KSAS Fall Conference, 2015. |
17 | Chatfield, A. B., Fundamentals of High Accuracy Inertial Navigation, Reston, VA, American Institute of Aeronautics and Astronautics, 1997. |
18 | Honeywell, Miniature Inertial Measurement Unit, 2006. |
19 | Northrop Grumman, LN-200s Inertial Measurement Unit, 2013. |
20 | Lorenz, R. D., "Radar Altimeters on Probes and Landers (and Doppler Radars)," 12th Interplanetary Probe Workshop, 2015. |