6Chang-Kyung Ryoo,Hangju Cho,Min-Jea Tahk.Time-to-go weighted optimal guidance with impact angle constraints.IEEE Transactions on Control Systems Technology,2006,14(3):483-492.
7Shigemune Taniwaki,YoshiakiOhkami.Precision attitude control of spacecraft with control moment gyros.Keystone,Colorado:AIAA Guidance,Navigation,and Control Conference and Exhibit,AIAA 2006-6801,2006.
8Ping Lu,David B.Doman,John D.Schierman.Adaptive terminal guidance for hypervelocity impact in specified direction.2005 AIAA Guidance,Navigation,andControl Conference and Exhibit,AIAA 2005-6059,2005.
9Byoung-Mun Min,Min-Jea Tahk,Byoung-Soo Kim,Hyo-Sang Shin.Guidance law for automatic landing of tilt-rotor aircraft.San Francisco,California:AIAA Guidance,Navigation,and Control Conference and Exhibit,AIAA 2005-6353,2005.
10In-Soo Jeon,Jin-Ik Lee,Min-Jea Tahk.Impact-time-control guidance law for anti-ship missiles.IEEE TRANSACTions on Control Systems Technology,2006,14(2):260-266.
2Nair D, Ag, garwal J K. Bayesian recognition of targets by parts in second generation forward looking infrared images. Image and Vision Computing, 2000, 18:849 - 864.
3Das S, Bhanu B. A system for model-based object recognition in perspective aerial images. Pattern Recognition, 1998, 31(4): 465--491.
4程国采，弹道导弹制导方法与最优控制，1987年
5钱杏芳，导弹飞行力学，1987年
6陈士橹，近代飞行器飞行力学，1987年
7王照林，近代控制理论基础，1983年
8Kim M, and Grider K V. oTerminal guidance for impact attitude angle constrained flight trajectoriesoIEEE Transactions on Aerospace and Electronic Systems, AES-9, Nov. 1973:852-859
9York R J. and Pastrick H L. oOptimal terminal guidance with constraints at final timeoJournal of Spacecraft and Rockets, ,June 1977: 381-382
10Glizer V Y. oOptimal planar interception with fixed end conditions: closed-form solutionoJournal of Optimization Theory and Applications, Mar. 1996:, 503-539
