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 品质规范
 qualities specification
 This paper describe necessity compiling carrier aircraft flying qualities specification according to needs of aviation development and inadequacies of Nation Military Standard (GJB185-86) at present. 根据我国航空事业发展的需要,以及现行国军标(GJB185—86)所存在的不足之处,论述了编制舰载飞机飞行品质规范的必要性。 短句来源 It presented some test results converted to standard conditions, and was compared with military helicopter handling qualities specification GJB902 - 90, and obtained objective flight test conclusion. 给出了换算到标准条件下的一些试验结果,并与军用直升机飞行品质规范CJB902-90的有关要求进行了对比,提出了客观的可供借鉴的试飞结论。 短句来源 This report gives a general discussion of the lateral-directional dynamic flying qualities of military airplanes, based mainly on the Military Flying Qualities Specification of Piloted aircraft, MIL-F-8785 B issued in 1969, to provide the necessary background for drafting the flying quality specification of our own country. 本文以美国1969年颁发的军用飞行品质规范MIL—F—8785B为中心,对横侧向动态飞行品质进行综合分析讨论,供引用国外规范的参考。 短句来源 PRELIMINARY STUDY OF FLYING QUALITIES SPECIFICATION OF SPACE SHUTTLE 航天飞机飞行品质规范初步研究 短句来源 The new progression of aircraft flying qualities specification 飞机飞行品质规范的新进展——对MIL-STD-1797的初步分析 短句来源 更多
 handling quality
 Currently, one of the hotspots in the research of helicopter flight control technology is to define performances of PCS based on handling quality standard, and to implement criteria requirements directly in PCS. 根据飞行品质规范确定飞控系统的性能要求、在飞控系统中直接实现规范要求，是目前直升机飞行控制技术研究的热点之一。 短句来源 The following conclusions have been drawn from this research program,:(1) The model following architecture allows for straightforward implementation of requirements of handling quality standard, and it can be utilized for helicopter handling quality design. (1)参考模型跟踪结构能够直接实现飞行品质规范要求，可以用于直升机飞行品质设计； 短句来源 After their dynamic responses in time domain are analyzed, augment stabilization controllers for the models are designed in terms of handling quality requirements by eigenvalue configuration technology. 在分析辨识模型的动态响应特性后 ,根据飞行品质规范的要求 ,采用极点配置技术对模型进行了增稳设计 ,并进行仿真验证。 短句来源
 quality specification
 The test results converted under standard conditions are given and compared with the relative requirements of the military helicopter flying quality specification HB6105-86. Lastly, the objective and reasonable conclusions have been drawn. 给出了换算到标准条件下的试验结果,并与军用直升机飞行品质规范HB6105-86的有关要求进行了比较,并得出了结论。 短句来源 This report gives a general discussion of the lateral-directional dynamic flying qualities of military airplanes, based mainly on the Military Flying Qualities Specification of Piloted aircraft, MIL-F-8785 B issued in 1969, to provide the necessary background for drafting the flying quality specification of our own country. 本文以美国1969年颁发的军用飞行品质规范MIL—F—8785B为中心,对横侧向动态飞行品质进行综合分析讨论,供引用国外规范的参考。 短句来源
 qualities specifications
 Airworthiness regulations, flying qualities specifications and design criterions 适航性条例、飞行品质规范和设计准则 短句来源 The handing qualities of aircraft for pitch axis are assessed using equivalent system criteria based on the flying qualities specifications(MIL STD 1797A). 在理解飞机飞行品质规范 MIL- STD- 1797A基础上 ,采用等效系统准则评价了某机的俯仰轴飞行品质。 短句来源 This paper, with reference to the data obtained from three Class-Ⅳ airplanes of the People's Republic of China, makes some comments on and analysises of the requirements of the lateral-directional dynamic qualities in Flying Qualities Specifications of the present U.S. piloted airplanes MIL-F-8785B (ASG) and the revisions recommended in reference [ 5 ]. 本文通过国内三架Ⅳ类飞机的计算数据和其它文献,对美国现行有人驾驶飞机的飞行品质规范MIL-F-8785B(ASG)的横航向动态飞行品质要求以及文献[5]对这些要求所提出的修改建议,进行了评述和研究。 短句来源 The paper proposes a design strategy based on state feedback and feedforward compensator for an inner loop of helicopter flight control system. This strategy is used to achieve the four independent channels tracking the given model. The desired model depends on the handling qualities specifications; 给出一种基于状态反馈与前置补偿的直升机飞控系统内回路设计策略,以实现内回路4个独立通道的隐模型跟踪,并根据操纵品质规范要求设计了期望的隐模型,使各通道实现了动态解耦及操纵解耦,且具有满意的动态跟踪响应特性,从而为简化外回路设计奠定了基础. 短句来源 A SUMMARY OF FLYING QUALITIES SPECIFICATIONS FOR DIRECT FORGE CONTROL AIRPLANES 直接力控制飞机飞行品质规范 短句来源 更多

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 qualities specification
 Fifteen rules are required to completely specify the Level 1 Short Term Response flying qualities specification for cruise flight conditions.
 handling quality
 Belleisle is a maincrop variety with good yield, exceptional table and handling quality. Handling quality requirements during data warehouse design involves allowing for distinct needs and domain visions of each stakeholder role. Honey extraction >amp; handling Quality control standards Honey testing kit Processing of honey. In the proposed QoS solution, differential services constitute a cornerstone for handling quality of service at the IP layer. Test flights of the prototype revealed even more handling quality issues than expected. 更多
 quality specification
 Analytical quality specification for measurements reported on an ordinal scale Therefore, the minimum quality specification for total error allowable is $${\it TE}_{\rm a} >amp;lt; 1.65(0.75\,CV_{\rm I} ) + {\rm }0.375\sqrt {\left( {\rm CV_{\rm I}} \right)^2 + \left( {\rm CV_{\rm G}} \right)^2 }$$ It also demonstrates how product quality specification such as surface roughness and machining process quality can be controlled by utilizing AFPNs. We perform algorithm/architecture co-design in which we meet high quality specification while keeping the power dissipation low. Analysis of plant historical data showed that the top quality specification was never exceeded whereas the bottom quality was somewhat erratic. 更多
 This report gives a general discussion of the lateral-directional dynamic flying qualities of military airplanes, based mainly on the Military Flying Qualities Specification of Piloted aircraft, MIL-F-8785 B issued in 1969, to provide the necessary background for drafting the flying quality specification of our own country.The lateral-directional mode characteristics is discussed first, followed by a discussion on lateral-directional dynamic response characteristics, the order being the same as that adopted... This report gives a general discussion of the lateral-directional dynamic flying qualities of military airplanes, based mainly on the Military Flying Qualities Specification of Piloted aircraft, MIL-F-8785 B issued in 1969, to provide the necessary background for drafting the flying quality specification of our own country.The lateral-directional mode characteristics is discussed first, followed by a discussion on lateral-directional dynamic response characteristics, the order being the same as that adopted by MIL-F-8785 B.In the discussion about mode characteristics, comparison is made between 8785 B and those specifications issued before 8785 B, such as 8785, AP970 and OTT, and explanation of the background for- the adoption of each criterion is given wherever possible.In the discussion about response characteristics, an analysis of the difference between 8785 B and "Proposed Revision to MIL-F-8785 B" (ref 5) is given. 本文以美国1969年颁发的军用飞行品质规范MIL—F—8785B为中心,对横侧向动态飞行品质进行综合分析讨论,供引用国外规范的参考。按MIL—F—8785B横向一航向飞行品质所采用的顺序,先讨论模态特性,再讨论动态反应特性。“在关于模态特性的讨论中,将8785B和在8785B以前颁发的规范如8785、AP970、OTT等进行比较,并尽可能说明所采用判据的依据。在关于动态反应特性讨论中,则着重分析8785B和文献5《对MIL—F—8785B的修改建议》之间的区别。 This paper, with reference to the data obtained from three Class-Ⅳ airplanes of the People's Republic of China, makes some comments on and analysises of the requirements of the lateral-directional dynamic qualities in Flying Qualities Specifications of the present U.S. piloted airplanes MIL-F-8785B (ASG) and the revisions recommended in reference [ 5 ]. The main contents are lateral-directional model characteristics, roll rate oscillations and sideslip excursion characteristics. 本文通过国内三架Ⅳ类飞机的计算数据和其它文献,对美国现行有人驾驶飞机的飞行品质规范MIL-F-8785B(ASG)的横航向动态飞行品质要求以及文献[5]对这些要求所提出的修改建议,进行了评述和研究。并提出了一些自己的看法。主要内容包括横航向模态特性、滚转速率振荡和侧滑幅值特性。 This paper makes a brief review of several phenomena of limit cycle oscillations appearing in some aircraft,and methods of theoretical analysis and experimental researches,and gives approximate relations between the limit cycle characteristics and the airplane-system parameters.It is,therefore,useful in the design of airplane stability and control for avoiding annoying limit cycle oscillation to satisfy the requirements of flying quality specifications. 本文综合介绍飞机上出现的各种极限环现象及其各种理论分析和实验研究的方法,给出极限环特性与飞机系统的一些参数之间的近似关系,对于飞机稳定性和操纵性设计中如何避免产生讨厌的极限环振荡,以满足飞行品质规范要求,具有一定的参考作用。 << 更多相关文摘
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