Integrated Flight and Thrust Control Design Based on Model-Following Control Method

飛控及推力整合之隨模控制法研究

鄭秋彬(Chiu-Pin Cheng) ； 歐陽讓(Jang Ouyang)

《中國航空太空學會學刊》 26卷3期 (1994/09) Pp. 211-222

https://doi.org/10.6124/TAASRC.199409_26(3).04

摘要

本文以保留縱向及橫向耦合的飛機模式進行引擎推力控制及飛行控制之整合設計研究。爲滿足傳統飛行控制設計規格，本文採用二階之理想模式配合隨模控制法進行設計。此設計不僅可提供較多的控制能量，在控制面失效時有較多的補償能力，而且在做高攻角飛行時，飛機亦有較強的穩定性。

關鍵字

飛行控制 ； 隨模控制 ； 耦合模式

並列摘要

An integrated flight and propulsion control system is developed based on the model-following control. This kind of system could greatly promote the maneuverability and enhance the survivability for high performance aircraft. All of the desired models are represented by second order systems and hence the classical design requirements could be guaranteed by the evaluation of the tracking performance. An 8×8 model of aircraft is developed. This model includes all the coupling effect between longitudinal axis and the lateral-directional axis, so the undersired coupling effect will be fixed during high angle of attack flight.

並列關鍵字

flight control ； model following control ； coupling model