| Year of publication |
2002 |
| Category |
Int. Conference |
| Subject |
|
| Title |
Optimal Guidance Laws with Terminal Impact Angle Constraint |
| Author |
유창경, 조항주, 탁민재 |
| Journal title |
Journal of Guidance, Control, and Dynamics |
| Publication date |
2005 |
| Volume & Other data |
Vol. 28, No. 4 |
| Abstract |
An optima 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 t_go-like function and the time varying guidance gain are studied. simulation studies show an excellent performance of the proposed guidance law. |
| Keywords |
|
| Issn Number |
|
| File |
 Optimal guidance for Missiles with Varying Velocity.pdf (433.7K) [14] DATE : 2015-10-01 13:56:59 |
