The subject invention provides for pitch, yaw and clockwise and counter clockwise roll control of a missile and more particularly but not by way of limitation to the use of a plurality of control panels which are slanted for controlling clockwise and counter clockwise roll of a missile.
Heretofore, there have been various types of missile control systems and arrangements such as drag controls, brake flaps and fins for controlling the operation of the missile. These devices and systems are disclosed in the following United States Patents: U.S. Pat. No. 2,793,591 to Jasse, U.S. Pat. No. 2,941,764 to Lee, Jr. et al, U.S. Pat. No. 2,942,545 to Fogal et al, U.S. Pat. No. 3,004,489 to Griffith et al, U.S. Pat. No. 3,114,315 to Trump, U.S. Pat. No. 3,174,430 to Apotheloz, U.S. Pat. No. 3,188,958 to Burke et al, U.S. Pat. No. 3,343,767 to Cafissi, U.S. Pat. No. 3,588,004 to Suter, U.S. Pat. No. 3,622,103 to Meier.
None of the above mentioned patents provide the unique features and advantages of the subject invention.