Analysis of optimal midcourse guidance law

IEEE Transactions on Aerospace and Electronic Systems

Volumn 32, Issue 1, 1996, Pages 419-425

  Yang, Shih Ming ^a  

^a NATIONAL CHENG KUNG UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION CONTROL; BOUNDARY CONDITIONS; BOUNDARY VALUE PROBLEMS; DRAG; FLIGHT DYNAMICS; LIFT; NAVIGATION; OPTIMAL CONTROL SYSTEMS; TRAJECTORIES;

ACCELERATION COMMAND; MIDCOURSE GUIDANCE LAW; THRUST;

MISSILES;

EID: 0029769827     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.481282     Document Type: Article

References (12)

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10. Speyer, J. L., Kim, K. D.Tahk, M. (1990) Passive homing missile guidance law based on new target maneuver models. Journal of Guidance, 13, 5 (1990), 803-812.
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12. Cherry, G. W. (1964) A general explicit, optimizing guidance law for rocket-propelled spaceflight. Paper 64-638, AIAA, New York, 1964.