| Title |
A Research of Attitude Angle Control Structure for Thrust Vector Control of Missiles at Initial Boosting Phase |
| Authors |
김부민(Kim, Boo-Min) ; 황익호(Whang, Ick-ho) |
| DOI |
https://doi.org/10.5370/KIEE.2017.66.10.1523 |
| Keywords |
Thrust Vectro Control ; Pitch Angle Control ; Pitch Rate Control |
| Abstract |
In general, the thrust vector control should be fast and stable in the initial launch phase. Two types of conventional controllers, one is for pitch angle control and the other is for pitch rate control, are designed based on the equation of motion without aerodynamics and are compared in the viewpoints of the stability margin and the time response performance. Also analyzed are the rejection capabilities to cope with high aerodynamic disturbances caused by high angle of attacks in initial booting phase. Additionally, time response features at actuator saturation are investigated. Based on those results, we suggest a controller structure which is more suitable for thrust vector control of missiles at initial booting phase. |