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7.4 - Challenges in Design and Development of Indigenous Flight Test Instrumentation System for a High Performance Fighter Aircraft

机译：7.4 - 用于高性能战斗机的土着飞行试验仪表系统的设计和开发的挑战

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V. Madhusudana Rao; K. Singh Chowhan; V. Patel; N. Prasad; P. Subramanyam;
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1. DEVELOPMENT OF AIRCRAFT STANDARD "FLOW SWITCH ASSEMBLY" (INDIGENOUSLY) FOR THE RADAR COOLING SYSTEM (RCS) OF TYPICAL FIGHTER AIRCRAFT [J] . L. Sheik Ismail, K. Nagaraja Journal of the Instrument Society of India: Proceedings of the national symposium on instrumentation . 2008,第1期

机译：典型战斗机雷达冷却系统（RCS）飞机标准“流量开关组件”的开发
2. INDIGENOUS DEVELOPMENT OF THE AIRCRAFT STANDARD "DUAL TEMPERATURE SENSOR" (THERMISTOR) FOR THE RADAR COOLING SYSTEM (RCS) OF TYPICAL FIGHTER AIRCRAFT [J] . K. Nagaraja Journal of the Instrument Society of India: Proceedings of the national symposium on instrumentation . 2006,第4期

机译：典型战斗机雷达冷却系统（RCS）的飞机标准“双温度传感器”（热敏电阻）的自主研发
3. Experimental Flight Testing of Night Vision Imaging Systems in Military Fighter Aircraft [J] . Roberto Sabatini, Mark A. Richardson, Maurizio Cantiello, Journal of testing and evaluation . 2014,第1期

机译：军用战斗机夜视成像系统的实验飞行测试
4. Challenges in Design and Development of Indigenous Flight Test Instrumentation System for a High Performance Fighter Aircraft [C] . V. Madhusudana Rao, Kishan Singh Chowhan, Vijay V. Patel, European Telemetry and Test Conference . 2014

机译：高性能战斗机的土着飞行试验仪表系统设计与开发的挑战
5. The development of an enhanced stability compensation design concept for a statically unstable fighter aircraft with a large stable pitching moment break at high angles of attack [D] . Lu, Cheng-Huei. 1989

机译：针对在高攻角下具有较大的稳定俯仰力矩中断的静态不稳定战斗机，增强了稳定性补偿设计概念的发展
6. Design and Evaluation of a Wireless Sensor Network Based Aircraft Strength Testing System [O] . Jian Wu, Shenfang Yuan, Genyuan Zhou, 2009

机译：基于无线传感器网络的飞机强度测试系统的设计与评估
7. Experimental flight testing of night vision imaging systems in military fighter aircraft [O] . Sabatini R, Richardson M, Cantiello M, 2014

机译：军用战斗机夜视成像系统的实验飞行试验

7.4 - Challenges in Design and Development of Indigenous Flight Test Instrumentation System for a High Performance Fighter Aircraft

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