Add to ORKGThe purpose of this project was to provide a means for operating the ailerons, elevator, elevator trim, rudder, nosewheel steering, and brakes in the Triton primary flight trainer. The main design goals under consideration were to illustrate system and subsystem integration, control function ability, and producibility. Weight and maintenance goals were addressed
NASA's current and projected advanced control technology programs for future transport aircraft incl...
The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...
The directions and speed of development of plane avionics systems are determined by three factors: e...
During the design of the C & P Aerospace Triton, a few problems were encountered that necessitated c...
Aircraft functional systems and crew systems were defined for a 1995 transport aircraft through a pr...
The goal of this project was to design, in detail, the wing, flaps, and ailerons for a primary fligh...
A compendium of stability augmentation system and autopilot block diagrams is presented. Descriptive...
The design of an integrated airframe/propulsion control system architecture is described. The design...
The Controls Group was assigned the responsibility for designing the Enabler's control system. The r...
The design, fabrication and flight testing of a powered elevator system for the Augmentor Wing Jet S...
Design requirements for the cabin, cabin system, flight controls, engine installation, and wing-fuse...
The analysis and preliminary design of an advanced technology transport aircraft flight control syst...
The active control technology (ACT) control/guidance system task of the integrated application of ac...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
Turbo-prop trainer aircraft are designed to offer a cost effective alternative to military jet train...
NASA's current and projected advanced control technology programs for future transport aircraft incl...
The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...
The directions and speed of development of plane avionics systems are determined by three factors: e...
During the design of the C & P Aerospace Triton, a few problems were encountered that necessitated c...
Aircraft functional systems and crew systems were defined for a 1995 transport aircraft through a pr...
The goal of this project was to design, in detail, the wing, flaps, and ailerons for a primary fligh...
A compendium of stability augmentation system and autopilot block diagrams is presented. Descriptive...
The design of an integrated airframe/propulsion control system architecture is described. The design...
The Controls Group was assigned the responsibility for designing the Enabler's control system. The r...
The design, fabrication and flight testing of a powered elevator system for the Augmentor Wing Jet S...
Design requirements for the cabin, cabin system, flight controls, engine installation, and wing-fuse...
The analysis and preliminary design of an advanced technology transport aircraft flight control syst...
The active control technology (ACT) control/guidance system task of the integrated application of ac...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
Turbo-prop trainer aircraft are designed to offer a cost effective alternative to military jet train...
NASA's current and projected advanced control technology programs for future transport aircraft incl...
The space shuttle digital, fly by wire, flight control system presents an interesting challenge in a...
The directions and speed of development of plane avionics systems are determined by three factors: e...