SOme control strategies of high angle of attack missile atuopilot

机译：高攻角自动驾驶仪的SOme控制策略

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Recent interest for missile high maneuverability and stealthness motivates new investigations in order to estimate potential and applicability of recent theoretical control methods and consequently to meet the industrial demands. SInce our work is closely related to an industrial application it is desirable to prijmarily deal with classical regulators. In the sequel, two nonlinear methods are considered: "Approximate feedbackj" linearization and asymptotic output tracking approach. Simulation results are given.

机译：最近对导弹的高机动性和隐身性的兴趣促使人们进行新的研究，以估计最新理论控制方法的潜力和适用性，从而满足工业需求。由于我们的工作与工业应用密切相关，因此最好先处理经典的调节器。在续篇中，考虑了两种非线性方法：“近似反馈”线性化和渐近输出跟踪方法。给出了仿真结果。

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来源
《4th IFAC(International Federation of Automatic Control) Symposium on Automatic Control in Aerospace 1998 Seoul, Korea, 24-28 August 1998》|1998年|p.53-58|共6页
会议地点 Seoul(KR)
作者
E.Devaud; S.Font; H.Siguerdidjane;
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原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
misile, nonlinear control; linearization; tracking; robustness.;

机译：导弹，非线性控制；线性化跟踪；健壮性。;

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3. Distributed synergetic guidance law for multiple missiles with angle-of-attack constraint [J] . You H., Zhao F-J The Aeronautical Journal . 2020,第1274期

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4. SOme control strategies of high angle of attack missile atuopilot [C] . E.Devaud, S.Font, H.Siguerdidjane International Federation of Automatic Control symposium on automatic control in aerospace . 1999

机译：高角度攻击导弹自动驾驶仪的控制策略
5. An experimental investigation of the physical mechanisms controlling the asymmetric flow past slender bodies at large angles of attack. [D] . Moskovitz, Cary A. 1989

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7. Three-Axis Autopilot Design for a High Angle-Of-Attack Missile Using Mixed H2/H∞Control [O] . Dae-Yeon Won, Min-Jea Tahk, Yoon-Hwan Kim 2010

机译：使用混合H2 /H∞Control的高角度导弹的三轴自动驾驶仪设计
8. A Preliminary Mehtod for Calculating the Aerodynamic Characteristics of Cruciform Missiles to High Angles of Attack Including Effects of Roll Angle and Control Deflections. [R] . nielsen,jack n. hemsch,michael j. 1978

机译：计算十字形导弹对大角度攻击气动特性的初步方法，包括侧倾角和控制偏差的影响。

SOme control strategies of high angle of attack missile atuopilot

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