[1] OUCHI K. Recent trend and advance of synthetic aperture radar with selected topics[J]. Remote Sensing, 2013, 5(2):716-727.
[2] MOREIRA A, IRAOLA P P, YOUNIS M, et al. A tutorial on synthetic aperture[J]. IEEE Geoscience and Remote Sensing Magazine, 2013, 1(1):6-43.
[3] KAHLE R, RUNGE H, ARDAENS J S, et al. Formation flying for along-track interferometric oceanography-First in-flight demonstration with TanDEM-X[J]. Acta Astronautica, 2014, 99:130-142.
[4] MOCCIA A, RUFINO G. Spaceborne along-track SAR interferometry:Performance analysis and mission scenarios[J]. IEEE Transactions on Aerospace and Electronic Systems, 2001, 37(1):199-213.
[5] 梁甸农, 蔡斌, 王敏, 等. 星载SAR-GMTI研究进展[J]. 国防科技大学学报, 2009, 31(4):87-92. LIANG D N, CAI B, WANG M, et al. Research process of spaceborne SAR-GMTI systems[J]. Journal of National Univeristy of Defense Technology, 2009, 31(4):87-92(in Chinese).
[6] MASSONNET D. Capabilities and limitations of the interferometric Cartwheel[J]. IEEE Transactions on Geoscience and Remote Sensing, 2001, 39(3):506-520.
[7] MOCCIA A, VETRELLA S. A tethered interferometric synthetic aperture radar (SAR) for a topographic mission[J]. IEEE Transactions on Geoscience and Remote Sensing, 1992, 30(1):103-109.
[8] BOMBARDELLI C, LORENZINI E C, QUADRELLI M B. Retargeting dynamics of a linear tethered interferometer[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(6):1061-1067.
[9] 钟睿, 徐世杰. 基于直接配点法的绳系卫星系统变轨控制[J]. 航空学报, 2010, 31(3):572-578. ZHONG R, XU S J. Orbit-transfer control for TSS using direct collocation method[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(3):572-578(in Chinese).
[10] 刘刚, 李传江, 马广富. 应用非线性模型预测控制的绳系卫星Halo轨道保持控制[J]. 航空学报, 2014, 35(9):2605-2614. LIU G, LI C J, MA G F. Station-keeping of tethered satellite system around a halo orbit using nonlinear model predictive control[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(9):2605-2614(in Chinese).
[11] WILLIAMS P, HYSLOP A, STELZER M, et al. YES2 optimal trajectories in presence of eccentricity and aerodynamic drag[J]. Acta Astronautica, 2009, 64(7):745-769.
[12] ZHONG R, ZHU Z H. Optimal control of nanosatellite fast deorbit using electrodynamic tether[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4):1182-1194.
[13] YU S H. Range-rate control algorithms and space rendezvous schemes[J]. Journal of Guidance, Control, and Dynamics, 1997, 20(1):206-208.
[14] GLABEL H, ZIMMERMANN F, BRUCKNER S, et al. Adaptive neural control of the deployment procedure for tether-assisted re-entry[J]. Aerospace Science and Technology, 2004, 8(1):73-81.
[15] WILLIAMS P. Optimal deployment/retrieval of tethered satellites[J]. Journal of Spacecraft and Rockets, 2008, 45(2):324-343.
[16] SUN G H, ZHU Z H. Fractional order tension control for stable and fast tethered satellite retrieval[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(6):2062-2066.
[17] ASLANOV V S, LEDKOV A S. Dynamics of tethered satellite systems[M]. Oxford:Woodhead Publishing, 2012:65-88.
[18] 徐鹤鸣. 多目标粒子群优化算法的研究[D]. 上海:上海交通大学, 2013:4-12. XU H M. Research on multi-objective particle swarm optimization algorithms[D]. Shanghai:Shanghai Jiao Tong University, 2013:4-12(in Chinese).
[19] 沈伋, 韩丽川, 沈益斌. 基于粒子群算法的飞机总体参数优化[J]. 航空学报, 2008, 29(6):1538-1541. SHEN J, HAN L C, SHEN Y B. Optimization of airplane primary parameters based on particle swarm algorithm[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(6):1538-1541(in Chinese).
[20] LEE N N, ZORN A H, WEST M. Passive vertical stabilization of two tethered nanosatellites with engineered damping[C]//AIAA/AAS Astrodynamics Specialist Conference and Exhibit. Reston:AIAA, 2008:1-16.
[21] LORENZINI E C. A three-mass tethered system for micro-g/variable-g applications[J]. Journal of Guidance, Control, and Dynamics, 1987, 10(3):242-249. |