| Patent Number |
Title Of Patent |
Date Issued |
| 6732974 |
Tiperon |
May 11, 2004 |
| A control surface for an air vehicle (e.g., an aircraft, rocket, or missile) is useful for flight control at both subsonic and supersonic speeds. The control surface defines the outboardmost tip of a flight structure (e.g., a wing, tail or other stabilizer) of the air vehicle. Hence, |
| 6580450 |
Vehicle internal image surveillance, recording and selective transmission to an active communica |
June 17, 2003 |
| A vehicle imaging surveillance and recording system adapted to monitor conditions prevailing during the course of a trip and provided for this purpose cameras are placed in the control station of the vehicle and about the vehicle. At least two recording devices record the output of the |
| 6247671 |
Ion doping apparatus and method for aerodynamic flow control |
June 19, 2001 |
| Method and apparatus for impingement on the sonic wave produced by a supersonic gas flow and the gas flow in a boundary layer of a gas that interfaces with a solid substrate comprising providing a source of a mixture of ions and electrons, introducing said ions and electrons into the |
| 5935177 |
Pilot-induced oscillation detection and compensation apparatus and method |
August 10, 1999 |
| The apparatus of this invention includes a pilot-induced oscillation (PIO) detector, a PIO compensator and a pilot input modifier. The PIO detector is coupled to receive aircraft state signal including the aircraft's pitch, roll and yaw attitudes. The PIO detector is also coupled to rece |
| 5850625 |
Sensor fusion apparatus and method |
December 15, 1998 |
| The invented apparatus fuses two or more sensor signals to generate a fused signal with an improved confidence of target existence and position. The invented apparatus includes gain, control and fusion units, and can also include an integration unit. The integration unit receives signals |
