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NTIS 바로가기Advances in space research : the official journal of the Committee on Space Research (COSPAR), v.68 no.11, 2021년, pp.4398 - 4417
Kwon, Dongyoung , Jung, Youyeun , Cheon, Yee-Jin , Bang, Hyochoong
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Automatica Açikmese 47 2 341 2011 10.1016/j.automatica.2010.10.037 Lossless convexification of a class of optimal control problems with non-convex control constraints
10.2514/6.2008-6426 Açikmese, B., Blackmore, L., Scharf, D.P., Wolf, A., 2008. Enhancements on the convex programming based powered descent guidance algorithm for Mars landing. In: AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Honolulu, HI, USA. AIAA Paper 2008-6426. doi: 10.2514/6.2008-6426.
J. Guidance Control Dyn. Açikmese 30 5 1353 2007 10.2514/1.27553 Convex programming approach to powered descent guidance for Mars landing
J. Guidance Control Dyn. Blackmore 33 1161 2010 10.2514/1.47202 Minimum-landing-error powered-descent guidance for Mars landing using convex optimization
J. Spacecraft Roc. Braun 44 2 310 2007 10.2514/1.25116 Mars exploration entry, descent and landing challenges
Braun, R.D., Powell, R.W., Cheatwood, F.M.N., et al., 1998. The Mars Surveyor 2001 lander: A first step toward precision landing. In: 49th International Astronautical Congress, Melbourne, AU. Paper IAF 98-Q.3.03.
J. Guidance Control Dyn. Dueri 40 2 197 2017 10.2514/1.G001480 Customized real-time interior-point methods for onboard powered-descent guidance
Space Sci. Rev. Golombek 211 5 2017 10.1007/s11214-016-0321-9 Selection of the InSight landing site
GR-CPCI-GR740-UM, 2019. GR-CPCI-GR740 Development Board 2019 User’s Manual (ver. 2.3).
GR740-UM-DS, 2020. GR740 Quad Core LEON4 SPARC V8 Processor 2020 Data Sheet and User’s Manual (vser. 2.4).
Grant, M., Boyd, S., 2020. CVX: MATLAB Software for Disciplined Convex Programming (ver. 2.2). URL: http://cvxr.com/cvx. [retrieved 27 Oct. 2020].
Guo, Y., Hawkins, M., Wie, B., 2011. Optimal feedback guidance algorithms for planetary landing and asteroid intercept. In: AAS/AIAA Astrodynamics Specialist Conference, Girdwood, AK, USA. AAS Paper 11-588.
J. Guidance Control Dyn. Guo 36 3 799 2013 10.2514/1.58098 Waypoint-optimized zero-effort miss/zero-effort-velocity feedback guidance for Mars landing
Hijorth, M., Aberg, M., Wessman, N.J., et al., 2016. GR740: Rad-hard quad-core LEON4FT system-on-chip. In: Eurospace DAta Systems in Aerospace, Tallinn, Estonia.
Proc. Inst. Mech. Eng., Part G: J. Aerospace Eng. Jung 230 11 2048 2015 10.1177/0954410015607893 Mars precision landing guidance based on model predictive control approach
J. Guidance Control Dyn. Liu 39 2 227 2016 10.2514/1.G001210 Entry trajectory optimization by second-order cone programming
Mao, Y., Szmuk, M., Xu, X., Açikmese, B., 2018. Successive convexification: A superlinearly convergent algorithm for non-convex optimal control problems arXiv preprint arXiv:1804.06539.
J. Guidance Control Dyn. Morgan 37 6 1725 2014 10.2514/1.G000218 Model predictive control of swarms of spacecraft using sequential convex programming
Int. J. Robot. Res. Morgan 35 1261 2016 10.1177/0278364916632065 Swarm assignment and trajectory optimization using variable-swarm, distributed auction assignment and sequential convex programming
ACM Trans. Mathe. Software (TOMS) Patterson 41 1 1 2014 10.1145/2558904 GPOPS-II: A MATLAB software for solving multiple-phase optimal control problems using hp-adaptive gaussian quadrature collocation methods and sparse nonlinear programming
Rush, B., Bhaskaran, S., Synnott, S.P., 2001. Improving Mars approach navigation using optical data. In: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference, San Diego, CA, USA. pp. 1651-1660.
J. Guidance Control Dyn. Scharf 40 2 213 2017 10.2514/1.G000399 Implementation and experimental demonstration of onboard powered-descent guidance
Optim. Methods Softw. Toh 11 1-4 545 1999 10.1080/10556789908805762 SDPT3: A MATLAB software package for semidefinite programming
J. Guidance Control Dyn. Wang 40 10 2603 2017 10.2514/1.G002150 Constrained trajectory optimization for planetary entry via sequential convex programming
J. Spacecraft Rock. Wang 55 4 993 2018 10.2514/1.A34102 Autonomous entry guidance for hypersonic vehicles by convex optimization
Adv. Astronaut. Sci. Wells 125 325 2006 Entry, descent and landing challenges of human Mars exploration
Aerosp. Sci. Technol. Zheng 45 359 2015 10.1016/j.ast.2015.06.008 Optimal nonlinear feedback guidance algorithm for Mars powered descent
Adv. Space Res. Zhou 54 11 2446 2014 10.1016/j.asr.2014.08.011 Improved ZEM/ZEV feedback guidance for mars powered descent phase
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