Interception Angle Control Guidance Using Proportional Navigation with Error Feedback

Journal of Guidance, Control, and Dynamics - Tập 36 Số 5 - Trang 1556-1561 - 2013
Chang-Hun Lee1, Tae-Hun Kim1, Min-Jea Tahk1
1Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea

Tóm tắt

Từ khóa


Tài liệu tham khảo

10.1109/TAES.1973.309659

Ben–AsherJ. Z.YaeshI., Advances in Missile Guidance Theory, Vol. 180, AIAA, Reston, VA, 1988, pp. 22–35.

10.2514/3.21541

10.2514/1.8392

10.2514/1.8392

10.2514/1.37864

10.2514/1.52105

10.1109/7.640285

10.1109/TCST.2005.863655

ZarchanP., Tactical and Strategic Missile Guidance, 2nd ed., AIAA, Washington, DC, 1994, pp. 45–66.

10.1137/0311001

10.2514/3.50527

GarnellP., Guided Weapon Control Systems, Pergamon Press, New York, 1980, p. 157.