Stuart C. Wright
31Patents
13h-index
19Co-inventors
78Inventor score
Filing activity: Mar 30, 1981 → Mar 31, 2011
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US5222691A | Automatic turn coordination trim control for rotary wing aircraft | Physics | 37 | Expired |
| US4816726A | Method of and arrangement for controlling and h-bridge electric motor | Electricity | 31 | Expired |
| US5224664A | Adaptive control system input limiting | Emerging Cross-Sectional Technologies | 29 | Expired |
| US4696445A | Collective control system for a helicopter | Performing Operations; Transporting | 25 | Expired |
| US5213282A | Maneuver feel system for a rotary wing aircraft | Physics | 17 | Expired |
| US4599698A | Aircraft trim actuator shutdown monitor system and method | Physics | 17 | Expired |
| US5299759A | Helicopter turn coordination and heading hold mode control | Physics | 17 | Expired |
| US5141177A | Model following control system | Physics | 17 | Expired |
| US5169090A | Attitude synchronization for model following control systems | Physics | 16 | Expired |
| US4626998A | Heading reference trim system | Physics | 16 | Expired |
| US4371937A | Retaining airspeed hold engagement in low speed maneuver | Physics | 15 | Expired |
| US4371939A | Roll attitude inhibit of aircraft coordinated turn disengagement | Physics | 14 | Expired |
| US4484283A | Aircraft roll-yaw fault protocols | Physics | 14 | Expired |
| US4392203A | Aircraft coordinated turn with lagged roll rate | Physics | 13 | Expired |
| US4580223A | Incorporation of pitch bias actuator function into an existing AFCS | Physics | 13 | Expired |
| US5178307A | High speed yaw control system for rotary wing aircraft | Physics | 13 | Expired |
| US4383299A | Command-inhibited aircraft attitude reference adjustment | Physics | 11 | Expired |
| US4577275A | Flight director go-around mode | Physics | 10 | Expired |
| US4594714A | Dual-actuator monitor | Physics | 9 | Expired |
| US4385356A | Non-saturating airspeed/attitude controls | Physics | 9 | Expired |
| US4387432A | Pulsed aircraft actuator | Physics | 9 | Expired |
| US4371938A | Automatic airspeed engage/disengage | Physics | 9 | Expired |
| US4371936A | Attitude trimmed airspeed/attitude controls | Physics | 8 | Expired |
| US4477876A | Dual response aircraft reference synchronization | Physics | 7 | Expired |
| US4385355A | Automatic outer loop centering of aircraft inner loop | Physics | 7 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.