|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/322 ; 244/321|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 21 인용 특허 : 0|
A control system for thrust vector controlled (TVC) cruciform missiles having only pitch and yaw thrusters is disclosed wherein roll damping feedback signals are generated from bank angle data in a separate feedback loop with appropriate gain and compensation. Additional roll rate compensation is added to the missile pitch and yaw rate control subsystem by multiplying actual roll rate by pitch and yaw control deflections and inserting the resultant roll rate compensation command in the pitch and yaw rate error control loops. The addition of these two con...
In a pitch and yaw rate subsystem of a thrust vector controlled (TVC) missile, a control system for damping actual roll rate solely by deflecting a pitch and yaw thrust vector nozzle, said subsystem producing pitch and yaw deflection rate commands for deflecting said thrust vector nozzle and having an inertial measurement unit (IMU) for providing signals representing actual pitch, yaw, and roll rates, said control system comprising: means for computing a bank angle from said IMU signals, said bank angle having a pitch component and a yaw component; selec...