Aircraft flight control system design under state and controlbounds

Lyshevski S.E.

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Aircraft flight control system design under state and controlbounds

机译：在状态和控制范围内的飞机飞行控制系统设计

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Sophisticated control configurations are needed to meet the mission and pilotage requirements for advanced aircraft. The required vehicle performance during low altitude, low speed and high angle of attack flight, all-weather, day and night operations must be achieved, and new control technologies should be developed. This work presents a systematic control design philosophy for flight control systems when the state variables and control inputs are bounded by the prespecified constraints. The design procedure uses the dynamic programming concept. The fundamental idea involves minimization of nonquadratic functionals. A new representation of constraints is proposed using the smooth functions. The advantages of the synthesis approach are presented. To illustrate the design methodology the longitudinal control configuration for the F-18 fighter is synthesized

机译：需要复杂的控制配置来满足高级飞机的任务和领航要求。在低空，低速和高攻角飞行，全天候，昼夜操作下，必须达到所需的车辆性能，并应开发新的控制技术。当状态变量和控制输入受预先规定的约束约束时，这项工作为飞行控制系统提出了系统的控制设计理念。设计过程使用动态编程概念。基本思想涉及最小化非二次函数。使用平滑函数提出了约束的新表示。提出了综合方法的优点。为了说明设计方法，综合了F-18战斗机的纵向控制配置

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《IEEE Transactions on Aerospace and Electronic Systems》 |1998年第1期|p.257-263|共7页
作者
Lyshevski S.E.;
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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
aircraft control; control system synthesis; dynamic programming; military aircraft; minimisation; stability; state feedback; F-18 fighter; advanced aircraft; aircraft flight control; attack flight; constraints; control bounds; control configurations; control inputs; dy;

机译：飞机控制;控制系统综合;动态编程;军用飞机;最小化;稳定性;状态反馈;F-18战斗机;先进飞机;飞机飞行控制;攻击飞行;约束条件;控制范围;控制配置;控制输入;dy;

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1. DESIGN OF ACTIVE CONTROL SYSTEM OF PASSENGER AIRCRAFT FOR ALLEVIATION OF EXTREME NEGATIVE LOAD FACTORS AT FLIGHT IN TURBULENT ATMOSPHERE USING LASER ATMOSPHERE SCANNING ALONG AIRCRAFT FLIGHT HEADING [J] . Vladimir Mikhailovich Kuvshinov, Grigoryi Andreevich Lazurin, Rim Maratovich Murzagalin TsAGI science journal . 2019,第6期

机译：乘法气扫描沿飞机航班扫描驾驶湍流大气飞行中极负荷因子激活控制系统设计
2. An alternative flight control system for an unmanned aircraft whose flight control system fails during a longitudinal flight with constant forward velocity [J] . Agneta M. BALINT, ?tefan BALINT INCAS Bulletin . 2010,第4期

机译：一种无人飞行器的替代性飞行控制系统，其飞行控制系统在恒定前进速度的纵向飞行过程中发生故障
3. Aircraft flight control system design under state and control bounds [J] . Lyshevski S.E. IEEE Transactions on Aerospace and Electronic Systems . 1998,第1期

机译：在状态和控制范围内的飞机飞行控制系统设计
4. Optimal tracking control of nonlinear dynamic systems with controlbounds [C] . Lyshevski S.E. Second IEEE International Software Engineering Standards Symposium, 1995. (ISESS'95) 'Experience and Practice', 1995 . 1995

机译：具有控制边界的非线性动力系统的最优跟踪控制
5. Damage-tolerant flight control system design for propulsion-controlled aircraft. [D] . Hitachi, Yoshitsugu. 2009

机译：推进控制飞机的容错飞行控制系统设计。
6. Integrated Flight Path Planning System and Flight Control System for Unmanned Helicopters [O] . Shau Shiun Jan, Yu Hsiang Lin 2011

机译：无人直升机的综合飞行路径计划系统和飞行控制系统
7. An alternative flight control system for an unmanned aircraft whose flight control system fails during a longitudinal flight with constant forward velocity [O] . Agneta M. BALINT, Ştefan BALINT 2010

机译：用于无人驾驶飞机的替代飞行控制系统，其飞行控制系统在纵向飞行期间以恒定的前进速度失效
8. Design and Flight Test of the Propulsion Controlled Aircraft (PCA) Flight ControlSystem on the NASA F-15 Test Aircraft [R] . Wells, E. A., Urnes, J. M. 1994

机译：美国宇航局F-15试验飞机上推进控制飞机（pCa）飞行控制系统的设计与飞行试验

Aircraft flight control system design under state and controlbounds

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