1) Bank-to-turn missile
倾斜转弯导弹
1.
This paper recommends simply the developing history of bank-to-turnmissile, the current programs and future vista at home or abroad,meanwhile,comments about key points and problem to be solved in guidance law ad autopilot of bank-to-turn missile.
本文简要地介绍了倾斜转弯导弹的发展史,国内外目前研究的状况以及发展前景。
2) bank-to-turn
倾斜转弯
1.
Against the character of the hypersonic vehicle bank-to-turn nonlinear controller,a more effective control method for nonlinear system was applied,which was nonlinear dynamic inversion technique.
高超声速飞行器的气动特性比一般的飞行器更为复杂,选用BTT(Bank-to-Turn)技术,即倾斜转弯技术可以满足其对于气动外形的要求,但随之给动力学系统带来了快时变、严重非线性及强烈耦合的特点。
2.
The design project of surface-to-air missiles offered in this paper which adopts a ramair engine and bank-to-turn(BTT) control technology has the property of a long range and high maneuverability.
为了满足远程高机动性要求,提出了将冲压发动机和倾斜转弯(BTT)控制技术应用于某型地空导弹的设计方法。
3.
A method of designing a bank-to-turn(BTT) flight control system of unmanned aerial vehicle(UAV) was studied to solve the problems cause by kinematics coupling,aerodynamic nonlinearity and parameter uncertainty.
研究无人机(UAV)的倾斜转弯(BTT)飞行控制系统的设计方法,解决UAV高机动倾斜转弯飞行时运动强烈耦合、气动特性强非线性和参数非定常性等特性带来的飞行控制系统设计难题。
3) BTT
倾斜转弯
1.
Bank-To-Turn (BTT) and Skid-To-Turn (STT) control techniques are widely used in current missile control systems.
现代导弹控制技术一般可分为侧滑转弯(Skid-to-Turn，STT)控制技术和倾斜转弯(Bank-to-Tum，BTT)控制技术。
2.
Bank-to-Turn (BTT) control technology has aroused wide concern among researchers in the design of the long-range guided weapons, powered by ramjet, with symmetrical structure.
倾斜转弯(BTT:Bank-to-Turn)控制技术在远程、采用冲压发动机、弹体具有面对称结构的制导武器的设计中受到了科研人员的广泛关注。
3.
Focused on the problem of reusable launch vehicle(RLV) attitude control,an engineering attitude control system based on the classical control theory and BTT technology was designed.
基于古典控制理论和BTT倾斜转弯控制技术,设计了可重复使用运载器(RLV)的大气层内姿态稳定控制系统。
4) bank-to-turn(BTT)
倾斜转弯(BTT)
5) BTT(bank-to-turn)
[军]倾斜转弯
6) k and turn indicator
倾斜转弯仪
补充资料：转弯倾斜仪
指示飞机的转弯方向和侧滑状况的飞行仪表。它由转弯仪和侧滑仪组成，是保证飞机正确盘旋和协调转弯的基本飞行仪表。转弯仪是最早（约1920年）得到实际应用的单自由度陀螺仪。陀螺内环轴支承在仪表壳体上。当飞机向左盘旋时，仪表壳体带动内环轴一起转动，使陀螺受到一个同方向的外力矩，根据陀螺的进动性的规则，陀螺立即绕内环轴进动，并通过倒向传动机构使指针偏向左边。陀螺进动的角度与盘旋角速度有关，因此，指针偏离中间的程度便反映出盘旋角速度的大小。为了避免指针摆动，表内还装有阻尼器，给内环轴以阻尼力矩。右盘旋时的工作原理完全一样，只是指针偏向右边。侧滑仪由弧形玻璃管和密封于其中的小球以及阻尼液组成。玻璃管固定在表盘上，飞机水平直线飞行时，小球位于玻璃管的中央。当飞机作正确盘旋时，作用在小球上的重力和离心力的合力方向与飞机竖轴一致，小球仍在中间位置，说明飞机无侧滑。当飞机有侧滑时，合力方向与飞机竖轴不一致，小球便偏离中间位置。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条