检索结果-内蒙古大学图书馆

QUASI-STEADY FLIGHT TO QUASI-STEADY FLIGHT TRANSITION FOR ABORT LANDING IN A WINDSHEAR - TRAJECTORY OPTIMIZATION AND GUIDANCE

引用

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1988年第2期58卷 165-207页

作者： MIELE, A WANG, T MELVIN, WW DELTA AIRLINES ATLANTAGA AIR LINE PILOTS ASSOC COMM AIRWORTHINESS & PERFORMANCEWASHINGTONDC

This paper is concerned with the optimal transition and the near-optimum guidance of an aircraft from quasi-steady flight to quasi-steady flight in a windshear. The abort landing problem is considered with reference t... 详细信息

关键词： Flight mechanics abort landing quasi-steady flight to quasi-steady flight transition optimal trajectories optimal control guidance strategies acceleration guidance gamma guidance feedback control windshear problems sequential gradient-restoration algorithm dual sequential gradient-restoration algorithm

来源：评论

学校读者我要写书评

暂无评论

OPTIMAL ABORT LANDING TRAJECTORIES IN THE PRESENCE OF WINDSHEAR

引用

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1987年第2期55卷 165-202页

作者： MIELE, A WANG, T TZENG, CY MELVIN, WW DELTA AIRLINES ATLANTAGA AIR LINE PILOTS ASSOC AIRWORTHINESS & PERFORMANCE COMMWASHINGTONDC

This paper is concerned with optimal flight trajectories in the presence of windshear. The abort landing problem is considered with reference to flight in a vertical plane. It is assumed that, upon sensing that the airplane is in a windshear, the pilot increases the power setting at a constant time rate until maximum power setting is reached; afterward, the power setting is held constant. Hence, the only control is the angle of attack. Inequality constraints are imposed on both the angle of attack and its time derivative.

关键词： Flight mechanics landing abort landing penetration landing optimal trajectories optimal control windshear problems sequential gradient-restoration algorithm dual sequential gradient-restoration algorithm

来源：评论

学校读者我要写书评

暂无评论

QUASI-STEADY FLIGHT TO QUASI-STEADY FLIGHT TRANSITION IN A WINDSHEAR - TRAJECTORY OPTIMIZATION AND GUIDANCE

引用

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1987年第2期54卷 203-240页

作者： MIELE, A WANG, T MELVIN, WW DELTA AIRLINES ATLANTAGA

This paper is concerned with the near-optimum guidance of an aircraft from quasi-steady flight to quasi-steady flight in a windshear. The take-off problem is considered with reference to flight in a vertical plane. In addition to the horizontal shear, the presence of a downdraft is considered. It is assumed that the power setting is held at the maximum value and that the aircraft is controlled through the angle of attack. Inequality constraints are imposed on both the angle of attack and its time derivative.

关键词： Flight mechanics take-off quasi-steady flight to quasisteady flight transition optimal trajectories optimal control guidance strategies feedback control windshear problems sequential gradient-restoration algorithm dual sequential gradient-restoration algorithm

来源：评论

学校读者我要写书评

暂无评论

GUIDANCE STRATEGIES FOR NEAR-OPTIMUM TAKE-OFF PERFORMANCE IN A WINDSHEAR

引用

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1986年第1期50卷 33-47页

作者： MIELE, A WANG, T MELVIN, WW DELTA AIRLINES ATLANTAGA AIR LINE PILOTS ASSOC AIRWORTHINESS & PERFORMANCE COMMWASHINGTONDC

This paper is concerned with guidance strategies for near-optimum performance in a windshear. This is a wind characterized by sharp change in intensity and direction over a relatively small region of space. The take-o... 详细信息

关键词： Guidance strategies gamma guidance theta guidance acceleration guidance flight mechanics take-off optimal trajectories optimal control feedback control windshear problems sequential gradient-restoration algorithm dual sequential gradient-restoration algorithm

来源：评论

学校读者我要写书评

暂无评论

OPTIMAL TAKE-OFF TRAJECTORIES IN THE PRESENCE OF WINDSHEAR

引用

JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS 1986年第1期49卷 1-45页

作者： MIELE, A WANG, T MELVIN, WW DELTA AIRLINES ATLANTAGA

This paper is concerned with optimal flight trajectories in the presence of windshear. With particular reference to take-off, eight fundamental optimization problems [Problems (P1)–(P8)] are formulated under the assumptions that the power setting is held at the maximum value and that the airplane is controlled through the angle of attack.

关键词： Piloting strategies flight mechanics take-off optimal trajectories optimal control windshear problems sequential gradient-restoration algorithm dual sequential gradient-restoration algorithm

来源：评论

学校读者我要写书评

暂无评论

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

请选择保存的检索档案：

请选择收藏分类：

通借通还

建议与咨询 留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

请选择保存的检索档案： 新增检索档案 确定 取消

请选择收藏分类： 新增自定义分类 确定 取消

通借通还

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

请选择保存的检索档案：

请选择收藏分类：