Exact Guidance Solution for Maneuvering Target on Relative Virtual Frame Formulation

Journal of Guidance, Control, and Dynamics - Tập 38 Số 7 - Trang 1330-1340 - 2015
In-Soo Jeon1, Hangju Cho2, Jin-Ik Lee3
1Antiship Systems Department, Agency for Defense Development, Daejeon 305-152, Republic of Korea
2Hanwha Corporation Research and Development Center, Daejeon 305-156, Republic of Korea
3Antiair Systems Department, Agency for Defense Development, Daejeon 305-152, Republic of Korea

Tóm tắt

Từ khóa


Tài liệu tham khảo

10.1109/TAES.1976.308328

10.1109/7.18664

10.1109/7.106131

10.2514/3.20828

10.2514/3.21109

10.2514/3.21685

10.1533/9781782420590.101

Ben-AsherJ. Z.YaeshI., Advances in Missile Guidance Theory, Vol. 180, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 1998, pp. 1–6.

10.1109/TAES.1972.309520

10.1109/7.102706

ZarchanP., Tactical and Strategic Missile Guidance, 4th ed., AIAA, Reston, VA, 2002, pp. 149–152.

10.2514/2.4240

Li C., 2007, Journal of the Japan Society for Aeronautical and Space Sciences, 50, 34

10.2514/1.8392

10.1109/TCST.2006.872525

10.1109/TAES.2007.357135

10.2514/3.50527

10.2514/1.14956

10.1109/TAES.2010.5595614

10.2514/3.21740

10.1109/TCST.2005.863655

10.2514/1.62910

10.2514/3.19880

10.1109/7.599315

10.2514/6.1997-3474

BrysonA. E.Jr.HoY. C., Applied Optimal Control, Hemisphere, New York, 1975, pp. 148–167.

GarnellP., Guided Weapon Control Systems, 2nd ed., Pergamon, Oxford, 1980, pp. 198–241.