1.The protective effect of two kinds of combined anti-G measures Ⅰ. anti-G suit (ATS) +positive-pressure breathing (PPB) ＋modified M-1 maneuver (mM-1 ), and Ⅱ. ATS＋PPB＋ L-1 maneuver were evaluated in 13 fighter pilots.
评价了13名歼击机飞行员实施两种综合抗荷措施（措施Ⅰ.抗荷服＋加压呼吸＋改良M－1动作和措施Ⅱ．抗荷服＋加压呼吸＋L－1动作）的防护效果。
2.With the combination of a 2nd - order adaptive model of maneuver detection and a 3rd -order adaptive model of maneuver level and a way of the interacting adaptive combination, it reaches "all-round" adaptive ability of tracking the various motions of a target.
它通过具有机动识别特性的二阶自适应模型和具有机动水平特性的三阶自适应模型,以及它们之间交互作用自适应组合方式的结合,达到了跟踪估计目标各种运动的“全面”自适应能力。
3.APPB_(5.98)+L—1 maneuver increased BP to a level higher than either APPB_(5.98) or L—1 maneuver used alone (p<0.05).
不论是否同时使用抗荷服,APPB_(5.98)+L-1动作的血压及预测G耐力均明显高于APPB_(5.98)及L-1动作单项措施,而且其疲劳程度与单纯使用L-1动作相比无明显差别。
4.Method Six male subjects using the new bladder anti G system were exposed to 10～15 s ladder shaped +Gz profiles without anti G straining maneuver(AGSM), then exposed to +5～9 Gz simulated aerial combat maneuver(SACM) with leg straining.
方法 6名男性被试者采用本囊式抗荷系统不做抗荷动作 (AGSM) ,暴露于 1 0～ 1 5s的梯形 +Gz曲线后 ,再暴露于 + 5～ 9Gz模拟空战动作曲线 (SACM ) ,并伴随腿部适度收紧。
5.QUASI-EULER-ANGLES FEEDBACK CONTROL OF SPACECRAFT ATTITUDE MANEUVER
航天器姿态机动的拟欧拉角反馈控制
6.Load matching (aerodynamic and maneuver loads) is investigated for turbojets and turbofans.
从多参数载荷谱的角度对发动机气动载荷与机动载荷的匹配进行了研究 ,针对不同构件给出了不同的多参数载荷谱的处理办法。
7.Venous hum is accentuated by deep inspiration in most patients and may be obliterated by the Valsalva maneuver or by pressure on the internal jugular vein.
多数病人在深吸气时静脉嗡鸣音明显，用瓦尔萨尔瓦手法或按压颈内静脉即或消除。
8.This paper designed fuzzy logic controller (FLC) applying in numerical simulations of two typical post-stall maneuvers such as trimmed and sustained flight up to 70 degree angle of attack and Cobra maneuver, after a mathematical model of aircraft was established and the specialties of fuzzy mathematics and fuzzy logic control were analyzed .
首先建立了进行过失速机动时飞机的动力学数学模型 ,并在分析了模糊数学和模糊逻辑控制特点的基础上 ,设计了模糊逻辑控制器 ( FLC)应用于 2种典型的过失速机动 ( 70°迎角定常飞行和眼镜蛇机动 )的数字仿真。
9.All ships use side thrusters and/or anti-gravity to maneuver, aerodynamic designs are out-of-place.
所有船都使用侧推进器和/或反引力来控制运动，空气动力学设计是不合适的。
10.Joint strategic maneuver is critical.
联合战略行动是决定性的。
