| 1. | Delay margin for predictive pi control system
控制系统的时滞稳定裕度 |
| 2. | With this method the system margin and system characteristics of atp gimbals control system can be improved
传递函数辨识方法应用于机架系统,改善了系统稳定裕度及系统特性。 |
| 3. | Gait with rith right stability margin is derived through many gaits simulation , experiments testifed the performance of the robot
得出稳定裕度合适的步态，实验验证了机器人的性能。 |
| 4. | The system introduces the preventive control that executes the emendation before the voltage violations , and it can increase the voltage security margin
另外系统还引入预防控制，在电压未越限时提前进行校正，提高了电压的稳定裕度。 |
| 5. | Then the effects of the grooved casing treatments on the performance of the compressor rotor have been revealed and some valuable conclusions have been reasoned out
通过对总性能和基元性能，特别是叶片尖部流动的详细测量，证明了这种型式的处理机匣可以提高效率，但在稳定裕度上略有损失，并解释了其影响转子性能的机理。 |
| 6. | 2 . decoupling performance and stability robustness are contradictory , we draw this conclusion by using stability margin ' s evaluation method which is based on the minimum singular value of return deference matrix for the multiva
2 、采用基于回差矩阵最小奇异值的稳定裕度求法，通过不同解耦方法的比较，得出结论：解耦性与鲁棒性是一对矛盾，设计时必须进行折衷处理。 |
| 7. | One is constant impedance modeling , the other is complicated load modeling . based on the time domain simulation , the sensitivity of stability margin with respect to node active and reactive power for the system with complicated load modeling is derived
结合时域仿真，本文提出了具有综合负荷模拟的暂态过程中发电机加速面积、减速面积、减速功率(稳定裕度)对网络节点有功、无功及变压器变比的灵敏度分析方法。 |
| 8. | The stability will fall when inlet flow is distorted . a circumferential critical distorted angle exists in the compressor , the stability of the compressor will change little when circumferential distorted angle is greater than critical distorted angle
进气畸变会使压气机的稳定性下降，但压气机存在一周向临界畸变角，当进气周向畸变区域大于周向临界畸变角时，压气机的稳定裕度和在临界畸变角时的相比，变化很小。 |
| 9. | In order to evaluate such characteristics as weight and static stability of proposed concepts effectively and conveniently during aircraft conceptual design , the implementation of center of gravity and associated weight estimation in an computer aided aircraft conceptual design system , whose data organization is object oriented , was studied
摘要为了在飞机概念设计阶段有效而便捷地评估方案重量和静稳定裕度等特性，研究了在一个按照面向对象方式进行数据组织的计算机辅助飞机概念设计系统中进行重心及相应重量估算的措施。 |
