tailless aircraft

A drag rudder is mostly used by tailless aircraft.

阻力方向舵在无尾飞机上得到广泛的应用.

Investigation of the direction control for the tailless aircraft configuration

无尾飞机布局方向控制特性研究

Characteristics of tailless aircraft wingtip stalling, including common and unique characteristics compared with other configurations, are analyzed with emphasis placed on the effect of wingtip stalling on flying qualities of tailless aircraft.

首先分析了无尾飞机翼尖失速的特点，包括与其他布局形式共有的和自身特有的特点，重点是翼尖失速对无尾飞机飞行品质的影响。

Analysis of Wingtip Stalling for Tailless Aircraft

无尾飞机翼尖失速问题研究

The dynamic simulation results indicate that the smart skin studied in the paper is able to maintain a sufficient authority to control the tailless aircraft in a low-rate maneuvering.

仿真结果表明，所讨论的智能蒙皮对机动要求不大的无尾飞行器具有足够的控制能力。

Adaptive Control for the Vertical Tailless Aircraft with Thrust Vectoring Control

无垂尾推力矢量飞机的自适应控制仿真研究

Design of LPV Gain-Scheduling Controller to Uncertain Tailless Aircraft

不确定性无尾飞行器LPV变增益控制器设计

In this paper a tailless aircraft was used as a model. Its dynamics was derived and the state-feedback controller was designed.

以无尾飞行器为例，推导了其动力学模型，并设计了状态反馈控制器。

Design Robust Mixed-Sensitivity Controller to Uncertain Tailless Aircraft

不确定性无尾飞行器混合灵敏度鲁棒控制器设计

Aircraft designers routinely use scale models, and in the case of the X-36 Tailless Fighter Agility Research Aircraft, that's as big as it got.

飞机设计师经常使用比例模型，并在案件的X-36战斗机敏捷性研究无尾飞机，这是因为大的，因为它得到了。

Blended-Wing-Body ( BWB) aircraft is a tailless large transport with high lift-drag ratio, and the aerodynamic study for BWB aircraft is a basis of overcoming the technology challenges about it. Firstly, research history on BWB configuration is presented in this paper;

翼身融合飞机（Blended Wing Body Aircraft-BWB Aircraft）是一种新型高升阻比无尾布局的大型运输机，其气动特性的研究是BWB布局飞机克服众多技术难题的基础。

Over the last seven decades, they've been a proving ground for developments including delta wings, tailless aircraft, and supersonic flight.

在过去的70年，他们已经为包括三角翼，无尾飞机发展的试验场，和超音速飞行。

In this paper are presented the major wind tunnel test results for the direction control of the tailless aircraft configuration.

介绍了无尾飞机布局方向控制特性风洞试验研究的主要结果。

Uncertain Tailless Aircraft Robust Gain-scheduling Controller Design Using LMI

基于LMI的不确定性无尾飞行器鲁棒变增益控制器设计