首页> 外文会议>AIAA aviation technology, integration and operations conference >Trajectory optimization algorithm for a constant altitude cruise flight with a required time of arrival constraints
【24h】

Trajectory optimization algorithm for a constant altitude cruise flight with a required time of arrival constraints

机译:轨迹优化算法,持续的海拔巡航飞行,所需的抵达时间约束

获取原文

摘要

Decreasing the flight costs, therefore flying along the optimal for a trajectory, is a constant preoccupation for all aircraft operators. Moreover, the reduction of fuel consumption and pollutant emissions is a significant factor in the trajectory optimization analysis. The study presented in this article is part of the research conducted at the Laboratoire de recherche en commande active, avionique et aeroservoelasticite (LARCASE), at Ecole de Technologie Superieure, in the field of aircraft trajectory optimization algorithms for Flight Management System platforms, and investigates an optimization algorithm for a leveled cruise flight segment with required time of arrival constraint. The proposed algorithm is deterministic, in accordance with the requirements for avionics equipment.
机译:从而减少飞行成本,因此沿着轨迹的最佳方式飞行,是所有飞机运营商的恒定关注。此外,减少燃料消耗和污染物排放是轨迹优化分析中的重要因素。本文提出的研究是在VillatoiredeChigherche en Commande Account,Avionique et Aeroservoelasticite(Larcase),在飞行管理系统平台的飞机轨迹优化算法领域的Avionique et Aeroservoelasticite(LARCASE)进行了研究的一部分,并调查具有达到到达时间约束的级别巡航飞行段的优化算法。根据航空电子设备的要求,所提出的算法是确定性的。

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