[1] WIE B, BAILEY D, HEIBERG C. Rapid multitarget acquisition and pointing control of agile spacecraft[J]. Journal of Guidance, Control, and Dynamics, 2002, 25(1):96-104.
[2] 靳瑾, 张景瑞, 刘藻珍. 航天器大角度姿态快速机动控制器参数优化设计[J]. 清华大学学报(自然科学版), 2009(2):289-292.JIN J, ZHANG J R, LIU Z Z. Optimized design of controller parameters for large angle spacecraft attitude maneuvers[J]. Journal of Tsinghua University (Science and Technology), 2009(2):289-292. (in Chinese)
[3] LEMAÎTRE M, VERFAILLIE G, JOUHAUD F, et al. Selecting and scheduling observations of agile satellites[J]. Aerospace Science and Technology, 2002, 6(5):367-381.
[4] CAO X, YUE C, LIU M, et al. Time efficient spacecraft maneuver using constrained torque distribution[J]. Acta Astronautica, 2016, 123:320-329.
[5] 印明威, 李京阳, 宝音贺西. 敏捷卫星姿态机动的奇异最优控制[J]. 光学精密工程, 2018, 26(4):906-915.YIN M W, LI J Y, BAOYIN H X. Singular optimal control for three-axis reorientation of an agile satellite[J]. Optics and Precision Engineering, 2018, 26(4):906-915. (in Chinese)
[6] YIN M, LI J, WANG X, et al. A rapid method for validation and visualization of agile earth-observation satellites scheduling[J]. Astrodynamics, 2018, 2(4):325-337.
[7] KARPENKO M, PROULX R J. Experimental implementation of Riemann-Stieltjes optimal control for agile imaging satellites[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(1):144-150.
[8] KING J T, KARPENKO M. A simple approach for predicting time-optimal slew capability[J]. Acta Astronautica, 2016, 120:159-170.
[9] KARPENKO M, BHATT S, BEDROSSIAN N, et al. First flight results on time-optimal spacecraft slews[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(2):367-376.
[10] KARPENKO M, BHATT S, BEDROSSIAN N, et al. Flight implementation of shortest-time maneuvers for imaging satellites[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4):1069-1079.
[11] 曾祥远, 龚胜平, 高云峰, 等. 非理想太阳帆航天器时间最优交会任务[J]. 清华大学学报(自然科学版), 2014, 54(9):1240-1244, 1254.ZENG X Y, GONG S P, GAO Y F, et al. Non-ideal solar sailcraft time-optimal rendezvous mission[J]. Journal of Tsinghua University (Science and Technology), 2014, 54(9):1240-1244, 1254. (in Chinese)
[12] 徐利民, 张涛. 基于外扰观测器的双通道航天器姿态控制方法[J]. 清华大学学报(自然科学版), 2017, 57(6):631-636.XU L M, ZHANG T. Dual channel spacecraft attitude control method based on an external disturbance observer[J]. Journal of Tsinghua University (Science and Technology), 2017, 57(6):631-636. (in Chinese)
[13] 程磊, 王天舒, 李俊峰. 挠性多体卫星姿态动力学与控制[J]. 清华大学学报(自然科学版), 2005, 45(11):1506-1509.CHENG L, WANG T S, LI J F. Attitude dynamics and control of a flexible multi-body satellite[J]. Journal of Tsinghua University (Science and Technology), 2005, 45(11):1506-1509. (in Chinese)
[14] YANG H W, LI S, BAI X L. Fast homotopy method for asteroid landing trajectory optimization using approximate initial co-states[J]. Journal of Guidance, Control, and Dynamics, 2019, 42(3):585-597.
[15] ROSS I M, KARPENKO M. A review of pseudospectral optimal control:From theory to flight[J]. Annual Reviews in Control, 2012, 36(2):182-197.
[16] KARPENKO M, KING J T, DENNEHY C J, et al. Agility analysis of the james webb space telescope[J]. Journal of Guidance, Control, and Dynamics, 2018, 10(1):1-12.
[17] BILIMORIA K D, WIE B. Time-optimal three-axis reorientation of a rigid spacecraft[J]. Journal of Guidance, Control, and Dynamics, 1993, 16(3):446-452.
[18] BAI X L, JUNKINS J L. New results for time-optimal three-axis reorientation of a rigid spacecraft[J]. Journal of Guidance, Control, and Dynamics, 2009, 32(4):1071-1076.
[19] FLEMING A, SEKHAVAT P, ROSS I M. Minimum-time reorientation of a rigid body[J]. Journal of guidance, control, and dynamics, 2010, 33(1):160-170.
[20] STEYN W H. Near-minimum-time eigenaxis rotation maneuvers using reaction wheels[J]. Journal of Guidance, Control, and Dynamics, 1995, 18(5):1184-1189.
[21] YU Y N, MENG X Y, LI K Y, et al. Robust control of flexible spacecraft during large-angle attitude maneuver[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(3):1027-1033.
[22] GILL P E, MURRAY W, SAUNDERS M A. SNOPT:An SQP algorithm for large-scale constrained optimization[J]. SIAM Review, 2005, 47(1):99-131.
[23] DARBY C L, HAGER W W, RAO A V. An hp-adaptive pseudospectral method for solving optimal control problems[J]. Optimal Control Applications and Methods, 2011, 32(4):476-502.
[24] PATTERSON M A, RAO A V. GPOPS-Ⅱ:A MATLAB software for solving multiple-phase optimal control problems using hp-adaptive Gaussian quadrature collocation methods and sparse nonlinear programming[J]. ACM Transactions on Mathematical Software (TOMS), 2014, 41(1):1-10.
[25] WIE B. Singularity escape/avoidance steering logic for control moment gyro systems[J]. Journal of Guidance, Control, and Dynamics, 2005, 28(5):948-956.
[26] 沈宏良, 曹万里, 刘昶. 飞机横向敏捷性的优化计算[J]. 飞行力学, 2002, 20(1):10-13.SHEN H L, CAO W L, LIU C. An optimal algorithm of calculating the roll agility for aircraft[J]. Flight Dynamics, 2002, 20(1):10-13. (in Chinese)