首页> 美国政府科技报告 >Manoeuvre Controller Design for an F-111C Flight Dynamics Model
【24h】

Manoeuvre Controller Design for an F-111C Flight Dynamics Model

机译:F-111C飞行动力学模型的机动控制器设计

获取原文

摘要

A maneuver controller program has been developed to fly an F-111C dynamic flight model through any number of prescribed maneuvers. A selection of discrete maneuvers is available which can be used as building blocks to represent most of those likely to be encountered in flight. Generalized maneuvers can also be flown by providing reference flight trajectories generated by an external source. The dynamic model and maneuver controller have been developed to allow the realistic modeling of maneuvers required by mission analyses, weapons delivery studies and systems assessments.

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

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