| Year of publication |
2003 |
| Category |
Int. Conference |
| Subject |
|
| Title |
Closed-Form Solutions of Optimal Guidance with Terminal Impact Angle Constraint |
| Author |
유창경, Hangju Cho, Min-Jea Tahk |
| Journal title |
Proceedings of the 2003 IEEE Int'l Conference on Control Application |
| Publication date |
June 23-25, 2003 |
| Volume & Other data |
Istanbul, Turkey |
| Abstract |
Optimal guidance laws and their closed-form solutions for controlling the impact angle as well as terminal miss are investigated in this paper. Generalized formulation of optimal guidance laws for constant speed missiles with a higher order system dynamics can be represented by a linear combination of a step and a ramp acceleration response of the missile. In the case of lag-free system, optimal guidance command is linear time varying and, therefore, the entire missile states can be expressed by polynomial functions in terms of time-to-go. We also proposed practical and precise time-to-go calculation methods in consideration of curved missile trajectory, which can be applied for various impact angle controllers. Basic properties including error analyses for the optimal guidance law for lag-free system are shown by numerical examples. |
| Keywords |
Impact angle control, Optimal guidance, Time-to-go estimation |
| Issn Number |
|
| Link |
 http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=1223469&tag [1546] |
