Three-dimensional guidance law with impact angle and impact time constraints

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 29, Issue 4, 2008, Pages 1020-1026

  Zhang, Youan ^a   Ma, Peibei ^a  

^a NAVAL AERONAUTICAL AND ASTRONAUTICAL UNIVERSITY   (China)

Author keywords

Impact angle; Impact time; Lyapunov stability; Navigation, guidance and control; Three dimensional guidance

Indexed keywords

CONTROL THEORY; FLIGHT DYNAMICS; KINEMATICS; LAWS AND LEGISLATION; MECHANICS; MILITARY EQUIPMENT; ORDNANCE; STABILITY; TARGETS; THREE DIMENSIONAL;

CIRCULAR ARCS; GUIDANCE LAW; IMPACT ANGLE; IMPACT ANGLES; IMPACT TIME; LINE-OF-SIGHT; LYAPUNOV STABILITY; LYAPUNOV STABILITY THEORY; NAVIGATION, GUIDANCE AND CONTROL; RELATIVE MOTIONS; SIMULATION RESULTS; THREE-DIMENSIONAL GUIDANCE; TIME PERIODS; TIME-TO-GO; TIME-VARYING;

MISSILES;

EID: 49549121820     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

1. Kim M, Grider K V. Terminal guidance for impact attitude angle constrained flight trajectories[J]. IEEE Transactions on Aerospace and Electronic Systems, 1973, 9(6): 852-859.
2. Song T L, Shin S J, Cho H. Impact angle control for planar engagements[J]. IEEE Transactions on Aerospace and Electronic Systems, 1999, 35(4): 1439-1444.
3. Kim B S, Lee J G, Han H S. Biased PNG law for impact with angular constraint[J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(6): 852-859.
4. Ryoo C K, Cho H J, Tahk M J. Closed-form solutions of optimal guidance with terminal impact angle constraint[C]//Proceedings of the 2003 Conference on Control Application. 2003: 504-509.
5. Jeon I S, Lee J I, Tahk M J. Impact-time-control guidance law for anti-ship missiles[J]. IEEE Transactions on Control Systems Technology, 2006, 14(2): 260-266.
6. Jeon I S, Lee J I, Tahk M J. Guidance law to control impact time and angle[C]//2006 International Conference on Control and Automation (ICCA2005). 2005: 852-857.
7. Jung B, Kim Y. Guidance laws for anti-ship missiles using impact angle and impact time[R]. AIAA-2006-6432, 2006.
8. Song S H, Ha I J. A Lyapunov-like approach to performance analysis of 3-dimensional pure PNG laws[J]. IEEE Transactions on Aerospace and Electronic Systems, 1994, 30(1): 239-247.