Controlling Sideslip Angle to Reduce the Radar Exposure of a Tactical, Rotary Winged UAV

This work investigates another way of contributing to the radar minimization solution for air vehicles in a threat environment. While muchresearch has been conducted on structural solutions to radar exposure minimization, not much work has been done in the area of using control tocontinuously assess and present the smallest radar cross section of an air vehicle to oncoming threat radar systems by changing the aircraft'sorientation. This work looks at the application of sideslip/beta angle f...