[1] K. AviDyne, "Guidance and Navigation for Entry Vehicles," under the cognizance of the Electronics Research Centernovamber 1968.
[2] J. C. Harpold, "Shuttle entry guidance," J. Astronaut. Sci., vol. 27, pp. 239-268, 1979.
[3] P. Lu and J. M. Hanson, "Entry guidance for the X-33 vehicle," Journal of Spacecraft and Rockets, vol. 35, pp. 342-349, 1998.
[4] G. J. Dominguez Calabuig and E. Mooij, "Optimal on-board abort guidance based on successive convexification for atmospheric re-entry," in AIAA Scitech 2021 Forum, 2021, p. 0860.
[5] G. Leng, "Guidance algorithm design: a nonlinear inverse approach," Journal of Guidance, Control, and Dynamics, vol. 21, pp. 742-746, 1998.
[6] M. Gräßlin, J. Telaar, and U. Schöttle, "Ascent and reentry guidance concept based on NLP-methods," Acta Astronautica, vol. 55, pp. 461-471, 2004.
[7] R. C. Wingrove, "Survey of atmosphere re-entry guidance and control methods," Aiaa Journal, vol. 1, pp. 2019-2029, 1963.
[8] J. Wang, Y. Tian, and Z. Ren, "Mixed guidance method for reentry vehicles based on optimization," Journal of Beijing University of Aeronautics and Astronautics, vol. 36, p. 736, 2010.
[9] Z. Liang and S. Zhu, "Constrained predictor-corrector guidance via bank saturation avoidance for low L/D entry vehicles," Aerospace Science and Technology, vol. 109, p. 106448, 2021.
[10] X. Lan, Z. Tan, T. Zou, and W. Xu, "CACLA-Based Trajectory Tracking Guidance for RLV in Terminal Area Energy Management Phase," Sensors, vol. 21, p. 5062, 2021.
[11] Z. Shen, On-board three-dimensional constrained entry flight trajectory generation: Iowa State University, 2002.
[12] Z. Dong, Y. Ren, K. Chen, and Y. Chen, "Research on Guidance and Control Law Design of Decelerating Transition and Vertical Landing for a STOVL UAV," in Journal of Physics: Conference Series, 2021, p. 012008.
[13] W. Zhi, Z. Ran, and L. Huifeng, "Hybrid Re-Entry Guidance for Reusable Launch Vehicle," Procedia Engineering, vol. 99, pp. 999-1004, 2015.
[14] R. Sarkar, J. Mukherjee, D. Patil, and I. N. Kar, "Re-entry trajectory tracking of reusable launch vehicle using artificial delay based robust guidance law," Advances in Space Research, vol. 67, pp. 557-570, 2021.
[15] M.-G. Seo, C.-H. Lee, and T.-H. Kim, "Trajectory shaping guidance law design using constraint-combining multiplier," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 235, pp. 1843-1853, 2021.
[16] E. CRAMER, J. BRADT, and J. HARDTLA, "NLP reentry guidance-Developing a strategy for low L/D vehicles," in Guidance, Navigation and Control Conference, 1988, p. 4123.
[17] F. J. Regan, Dynamics of atmospheric re-entry: Aiaa, 1993.
[18] P. Lu, "Entry guidance: a unified method," Journal of Guidance, Control, and Dynamics, vol. 37, pp. 713-728, 2014.
[19] K. Bollino, M. Ross, and D. Doman, "Optimal nonlinear feedback guidance for reentry vehicles," in AIAA guidance, navigation, and control conference and exhibit, 2006, p. 6074.
[20] R. Esmaelzadeh, A. Naghash, and M. Mortazavi, "Near optimal re-entry guidance law using inverse problem approach," Inverse Problems in Science and Engineering, vol. 16, pp. 187-198, 2008.
[21] P. Zarchan, "Tactical and Strategic Missile Guidance Fourth Edition," PROGRESS IN ASTRONAUTICS AND AERONAUTICS, vol. 199, 2002.
[22] N. A. Shneydor, Missile guidance and pursuit: kinematics, dynamics and control: Elsevier, 1998.
[23] P. J. Shaffer, I. M. Ross, M. W. Oppenheimer, D. B. Doman, and K. P. Bollino, "Optimal Trajectory Reconfiguration and Retargeting for Reusable Launch Vehicles," Journal of Guidance, Control, and Dynamics, vol. 30, pp. 1794-1802, 2007.
[24] Z. Jiang, J. Ge, Q. Xu, and T. Yang, "Impact Time Control Cooperative Guidance Law Design Based on Modified Proportional Navigation," Aerospace, vol. 8, p. 231, 2021.
[25] M. A. Masoumnia, M. B. Menhaj, and A. Sooratgar, "A unified structure for basic guidance laws of moving objects," International Journal of Systems Science, vol. 52, pp. 2647-2659, 2021.
[26] E. Hensel, Inverse theory and applications for engineers: Prentice Hall, 1991.
[27] P. Parvathy and J. Jacob, "Inverse Optimal Control Via Diagonal Stabilization Applied to Attitude Tracking of a Reusable Launch Vehicle," Journal of Optimization Theory and Applications, vol. 191, pp. 794-822, 2021.
[28] X. Guoqiang, "Launch Vehicle Reconfigurable Guidance Method Based on Online Trajectory Optimization," 中国航天 (英文版), vol. 22, pp. 20-27, 2021.
[29] J.-J. E. Slotine and W. Li, Applied nonlinear control vol. 199: Prentice hall Englewood Cliffs, NJ, 1991.
[30] O. A. Yakimenko, "Direct method for rapid prototyping of near-optimal aircraft trajectories," Journal of Guidance, Control, and Dynamics, vol. 23, pp. 865-875, 2000.
[31] D. B. Doman and M. W. Oppenheimer, "Integrated Adaptive Guidance and Control for Space Access Vehicles, Volume 1: Reconfigurable Control Law for X-40A Approach and Landing," AFRL IAG&C Technical Report.
[32] P. J. Shaffer, "Optimal trajectory reconfiguration and retargeting for the X-33 reusable launch vehicle," NAVAL POSTGRADUATE SCHOOL MONTEREY CA2004.
[33] G. Chen, L.-l. Dong, G.-r. Yan, M. Xu, and S.-l. Chen, "Recent status and development review of spacecraft reentry guidance methods," FLIGHT DYNAMICS-XIAN-, vol. 26, p. 1, 2008.
[34] v. s. Lobanov, "Reentry Guidance Algorithms of Space Vehicles in the Earth Atmosphere," presented at the AIAA Guidance, Navigation, and Control Conference, 2002.
[35] W. Qing, R. Maopeng, and Z. Yang, "Reentry Guidance for Hypersonic Vehicle Based on Predictor⁃ Corrector Method," Journal of Beijing University of Aeronautics and Astronautics, vol. 39, p. 1563, 2013.
[36] M. Mortazavi, "Trajectory determination using inverse dynamics and reentry trajectory optimization," Ph. D. Thesis, Moscow Aviation Institute, 2000.
[37] R. Esmaelzadeh, A. Naghash, and M. Mortazavi, "An Explicit Reentry Guidance Law Using Bezier Curves," Transactions of the Japan Society for Aeronautical and Space Sciences, vol. 50, pp. 225-230, 2008.
[38] A. Naghash, R. Esmaelzadeh, M. Mortazavi, and R. Jamilnia, "Near optimal guidance law for descent to a point using inverse problem approach," Aerospace Science and Technology, vol. 12, pp. 241-247, 2008.
[39] N. Mahmoodian, "Guidance and Control in Reentry Guidance based on Nominal Trajectory Tracking," MS Thesis, KNT University of Technology ( In Persian), 2001.
[40] S.-Y. LIU, Z.-X. LIANG, Z. REN, and Q.-D. LI, "Review of reentry guidance methods for hypersonic gliding vehicles," Chinese Space Science and Technology, vol. 36, p. 1, 2016.
[41] F. Marchetti and E. Minisci, "Genetic programming guidance control system for a reentry vehicle under uncertainties," Mathematics, vol. 9, p. 1868, 2021.
[42] L. Zang, D. Lin, S. Chen, H. Wang, and Y. Ji, "An on-line guidance algorithm for high L/D hypersonic reentry vehicles," Aerospace Science and Technology, vol. 89, pp. 150-162, 2019.
[43] H. Wang, M. Gu, Q. Yu, Y. Tao, J. Li, H. Fei, et al., "Adaptive and large-scale service composition based on deep reinforcement learning," Knowledge-Based Systems, vol. 180, pp. 75-90, 2019.
[44] L.-s. He and D.-j. Xu, "Optimal trajectory and heat load analysis of different shape lifting reentry vehicles for medium range application," Defence Technology, vol. 11, pp. 350-361, 2015.
[45] K.-Y. Tu, M. S. Munir, K. D. Mease, and D. S. Bayard, "Drag-based predictive tracking guidance for Mars precision landing," Journal of Guidance, Control, and Dynamics, vol. 23, pp. 620-628, 2000.
[46] S. Ishimoto, "Nonlinear entry trajectory control using drag-to-altitude transformation," Journal of Guidance, Control, and Dynamics, vol. 23, pp. 378-380, 2000.
[47] F. Marchetti, E. Minisci, and A. Riccardi, "Single-stage to orbit ascent trajectory optimisation with reliable evolutionary initial guess," Optimization and Engineering, pp. 1-26, 2021.
[48] A. Abbadi, R. Matousek, P. Osmera, and L. Knispel, "Spatial guidance to RRT planner using cell-decomposition algorithm," in 20th international conference on soft computing, MENDEL, 2014.
[49] Y. Wu, B. Yan, and X. Qu, "Improved chicken swarm optimization method for reentry trajectory optimization," Mathematical Problems in Engineering, vol. 2018, 2018.
[50] P. Cheng, Z. Shen, and S. M. LaValle, "RRT-based trajectory design for autonomous automobiles and spacecraft," Archives of control science, vol. 11, pp. 167-194, 2001.
[51] E. Frazzoli, M. A. Dahleh, and E. Feron, "Real-time motion planning for agile autonomous vehicles," Journal of guidance, control, and dynamics, vol. 25, pp. 116-129, 2002.
[52] G. Barton and S. Tragesser, "Autolanding trajectory design for the X-34," in 24th Atmospheric Flight Mechanics Conference, 1999, p. 4161.
[53] A. C. Grubler, "New methodologies for onboard generation of terminal area energy management trajectories for autonomous reusable launch vehicles," Massachusetts Institute of Technology, 2001.
[54] G. H. Barton, A. C. Grubler, and T. R. Dyckman, "New methodologies for onboard generation of TAEM trajectories for autonomous RLVs," in 2002 core technologies for space systems conference, 2002.
[55] Ü. Dinçer and M. Çevik, "Improved trajectory planning of an industrial parallel mechanism by a composite polynomial consisting of Bézier curves and cubic polynomials," Mechanism and Machine Theory, vol. 132, pp. 248-263, 2019.
[56] B. Zhang and D. Zhu, "A new method on motion planning for mobile robots using jump point search and Bezier curves," International Journal of Advanced Robotic Systems, vol. 18, p. 17298814211019220, 2021.
[57] V. Norman-Gerum and J. McPhee, "Constrained dynamic optimization of sit-to-stand motion driven by Bézier curves," Journal of biomechanical engineering, vol. 140, 2018.
[58] C. Scheiderer, T. Thun, and T. Meisen, "Bezier curve based continuous and smooth motion planning for self-learning industrial robots," Procedia Manufacturing, vol. 38, pp. 423-430, 2019.
[59] K. Judd and T. McLain, "Spline based path planning for unmanned air vehicles," in AIAA Guidance, Navigation, and Control Conference and Exhibit, 2001, p. 4238.
[60] H. Duan and S. Li, "Artificial bee colony–based direct collocation for reentry trajectory optimization of hypersonic vehicle," IEEE Transactions on Aerospace and Electronic Systems, vol. 51, pp. 615-626, 2015.
)