首页> 外国专利> Guidance control device for vertical take-off plane, vertical takeoff landing gear, guidance control method of vertical takeoff landing machine, and guidance control program of vertical takeoff landing gear

Guidance control device for vertical take-off plane, vertical takeoff landing gear, guidance control method of vertical takeoff landing machine, and guidance control program of vertical takeoff landing gear

机译:用于垂直起飞平面的引导控制装置,垂直起飞升降机,垂直起飞升降机的引导控制方法,以及垂直起飞升降机的指导控制程序

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
机译:要解决的问题:提供一种指导控制装置,其允许进行自动引导飞行,以便执行速度命令,升序和下降率命令和标题命令的输入,并进一步涵盖了整个过渡领域的自动指导飞行在其中倾斜角度和飞行速度等的航班。;解决方案:用于垂直起飞和着陆飞机的引导控制装置30包括:垂直引导规则生成部分32a,它产生音高姿态角度命令和节气门命令根据使用模式参数的反馈引导控制,该模式参数与机身34的模式的变化有关,从AirFrame 34的第一状态参数,输入的升序和降序命令和提升速度命令;和横向/方向引导规则生成部分32b,其根据使用模式参数的反馈引导控制生成滚动姿态角度命令和偏航棒命令,从AirFrame 34的第二状态参数,输入的标题命令和横向进步命令。;所选绘图:图4;版权:(c)2019,JPO和INPIT

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号