GUIDANCE CONTROL DEVICE FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT, VERTICAL TAKE-OFF AND LANDING AIRCRAFT, GUIDANCE CONTROL METHOD FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT, AND GUIDANCE CONTROL PROGRAM FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT

摘要

PROBLEM TO BE SOLVED: To provide a guidance control device which allows automatic guidance flights to be performed that follow an input of speed commands, ascending and descending rate commands, and heading commands, and which further covers automatic guidance flights in the whole area of transition flights during which tilt angles and flight speed or the like change.;SOLUTION: A guidance control device 30 for a vertical take-off and landing aircraft comprises: a vertical guidance rule generation section 32a which generates pitch attitude angle commands and throttle commands, in accordance with feedback guidance control using mode parameters related to changes in modes of an airframe 34, from a first state parameter of the airframe 34, inputted ascending and descending rate commands, and advancement speed commands; and a lateral/direction guidance rule generation section 32b which generates roll attitude angle commands and yaw stick commands, in accordance with feedback guidance control using the mode parameters, from a second state parameter of the airframe 34, inputted heading commands, and lateral advancement commands.;SELECTED DRAWING: Figure 4;COPYRIGHT: (C)2019,JPO&INPIT