Title :
Sidestick controllers for advanced aircraft cockpits
Author :
Hegg, Jeffrey W. ; Smith, Marion P. ; Yount, Larry
Author_Institution :
Honeywell Inc., Clearwater, FL, USA
Abstract :
Utilization of sidestick controllers for pitch and roll is examined for advanced cockpit configurations for commercial transport aircraft. Specifically, information on active sidesticks which are servo coupled for dual sidestick cockpit configurations is presented. Hardware development status is presented along with results of evaluations. The sticks are coupled such that when one of them is displaced the other one will track that displacement. Autopilot or flight control inputs will cause each stick to displace, thereby providing a visual cue on how much control authority is being implemented. The autopilot can be overridden by applying pressure to the stick or pressing a disengage button on the grip. The sidesticks incorporate the following feel features: break-out forces, linear force gradients, softstop steps, and hardstops. The softstop-to-hardstop region provides a tactile cue to tile pilot that stick displacement limits are being reached and provides the capability of modifying the control laws in this region of sidestick displacement when approaching the aircraft limitations
Keywords :
aerospace computer control; aircraft control; electric control equipment; servomechanisms; active sidesticks; advanced aircraft cockpits; autopilot; break-out forces; closed loop system; commercial transport aircraft; displacement; dual sidestick cockpit configurations; flight control; linear force gradients; pitch and roll; servo coupled sidestick; sidestick controllers; sidestick displacement; softstop steps; visual cue; Aerospace control; Aerospace electronics; Aircraft; Control systems; Displacement control; Force control; Motion control; Proportional control; Servomechanisms; Servomotors;
Conference_Titel :
Digital Avionics Systems Conference, 1992. Proceedings., IEEE/AIAA 11th
Conference_Location :
Seattle, WA
Print_ISBN :
0-7803-0820-4
DOI :
10.1109/DASC.1992.282112