| Year of publication |
1996 |
| Category |
Int. Conference |
| Subject |
|
| Title |
Closed-Form Optimal Guidance Law for Missiles of Time-Varying Velocity |
| Author |
Hangju cho, 유창경, Min-Jea Tahk |
| Journal title |
Journal of Guidance, Control, and Dynamics |
| Publication date |
1996 |
| Volume & Other data |
Vol. 19, No. 5 |
| Abstract |
An optimal guidance law for missiles with time-varying velocity is investigated. The closed-form solution is derived and properties of the key variables of the solution, such as a time-to-go-like function and the time-varying guidance gain, are studied. Implementation aspects related to the computations of time-to-go and the guidance gain also are considered. Simulation studies show that the performance of the proposed guidance law is superior to that of proportional navigation or augmented proportional navigation. |
| Keywords |
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| Issn Number |
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| File |
 Closed-form optimal guidance law for missiles of time-varying velocity.pdf (361.7K) [12] DATE : 2015-10-01 13:40:49 |
