[1] CHEN S Y, XIA Q L. A Multiconstrained ascent guidance method for solid rocket-powered launch vehicles[J]. International Journal of Aerospace Engineering, 2016(1):1-11. [2] QUADRELLI M B, WOOD L J, RIEDEL J E, et al. Guidance, navigation, and control technology assessment for future planetary science missions[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(7):1165-1186. [3] VACHON A, DESBIENS A, GAGNON E, et al. Launch ascent guidance by discrete multi-model predictive control[J]. Acta Astronautica, 2014, 95:101-110. [4] HULL D G, HARRIS M W. Optimal solutions for quasiplanar ascent over a spherical Moon[J]. Journal of Guidance, Control and Dynamics, 2012, 35(4):1218-1223. [5] LU P, FORBES S, BALDWIN M. A versatile powered guidance algorithm[C]//AIAA Guidance, Navigation, and Control Conference. Reston, VA:AIAA, 2012:4843-4858. [6] JEB S O, JOHN H W, TANNEN S V, et al. Space launch system ascent flight dontrol design[DB/OL].http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20140008731.pdf. [7] LAN X J, LIU L, WANG Y J. Online trajectory planning and guidance for reusable launch vehicles in the terminal area[J]. Acta Astronautica, 2016, 118:237-245. [8] HALBE O, RAJA R G, PADHI R. Robust reentry guidance of a reusable launch vehicle using model predictive static programming[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(1):134-148. [9] SONG E J, CHO S, ROH W R. A comparison of iterative explicit guidance algorithms for space launch vehicles[J]. Advances in Space Research, 2015, 55(1):463-476. [10] TIAN B, FAN W, SU R, et al. Real-time trajectory and attitude coordination control for reusable launch vehicle in reentry phase[J]. IEEE Transactions on Industrial Electronics, 2015, 62(3):1639-1650. [11] LU B, CUI N, FU Y, et al. Closed-loop atmospheric ascent guidance based on finite element method[J]. Aircraft Engineering and Aerospace Technology:An International Journal, 2015, 87(5):393-401. [12] 陈新民, 余梦伦. 迭代制导在运载火箭上的应用研究[J]. 宇航学报, 2003, 24(5):484-489. CHEN X M, YU M L. Study of iterative guidance application to launch vehicles[J]. Journal of Astronautics, 2003, 24(5):484-489(in Chinese). [13] 茹家欣. 液体运载火箭的一种迭代制导方法[J]. 中国科学E辑:技术科学, 2009, 39(4):696-706. RU J X. An iterative guidance method for liquid launch vehicle[J]. Science in China Series E:Technological Sciences, 2009, 39(4):696-706(in Chinese). [14] 池贤彬, 岳晓奎, 李鹏. 基于凸优化的自主交会迭代制导方法[J]. 中国空间科学技术, 2014(1):26-34. CHI X B, YUE X K, LI P, et al. Iterative guidance method of autonomous rendezvous based on convex optimization[J]. Chinese Space Science & Technology, 2014(1):26-34. [15] LU P, GRIFFIN B J, DUKEMAN G A, et al. Rapid optimal multiburn ascent planning and guidance[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(6):1656. [16] LU P, SUN H, TSAI B. Closed-loop endoatmospheric ascent guidance[J]. Journal of Guidance Control and Dynamics, 2003, 26(2):283-294. [17] LU P, PAN B. Highly constrained optimal launch ascent guidance[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(2):404-414. [18] 傅瑜, 陈功, 卢宝刚,等. 基于最优解析解的运载火箭大气层外自适应迭代制导方法[J]. 航空学报, 2011, 32(9):1696-1704. FU Y, CHEN G, LU B G, et al. A vacuum adaptive iterative guidance method of launch vehicle based on optimal analytical solution[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(9):1696-1704(in Chinese). [19] 郑旭, 高长生, 陈尔康,等. 一种基于大气层外解析动力学模型的最优迭代制导方法[J]. 西北工业大学学报, 2016, 34(6):1093-1100. ZHENG X, GAO C S, CHEN E K, et al. An optimal iterative guidance method based on exoatmospheric analytical dynamic model[J]. Journal of Northwestern Polytechnical University, 2016, 34(6):1093-1100(in Chinese). [20] 邓逸凡, 李超兵, 王志刚. 一种基于轨道要素形式终端约束的航天器空间变轨迭代制导算法[J]. 航空学报, 2015, 36(6):1975-1982. DENG Y F, LI C B, WANG Z G. An iterative guidance algorithm using orbital elements as terminal constraints for spacecraft orbit transfer[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(6):1975-1982(in Chinese). [21] 李超兵, 王晋麟, 李海. 一种基于多终端约束的最优制导方法[J]. 中国空间科学技术, 2016, 36(5):9-17. LI C B, WANG J L, LI H. An optimal guidance method based on multiple terminal constraints[J]. Chinese Space Science and Technology, 2016, 36(5):9-17(in Chinese). |