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Synonyms were used for: autopilot
Search without synonyms: keywords:(missile autopilot)

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    Longitudinal nonlinear adaptive autopilot design for missiles with control constraint

    Lee, Keum W / Singh, Sahjendra N | SAGE Publications | 2018
    Keywords: Adaptive missile autopilot , longitudinal autopilot with input constraints , nonlinear missile control

    Design of Missile Autopilot with Aerodynamic Lift and Reaction Jets Based on Auto Disturbance Rejection Controller

    Yang, Chong / Zhang, Ke / Lu, Mei-Bai | Tema Archive | 2012
    Keywords: Autopilotsystem , missile autopilot , interceptor missile

    A dimension reduction observer-based guidance law accounting for dynamics of missile autopilot

    Qu, Pingping / Zhou, Di | SAGE Publications | 2013
    Keywords: Missile , autopilot

    A generalized design method for three-dimensional guidance laws

    Sun, Sheng / Zhou, Di / Zhou, Jingyang et al. | SAGE Publications | 2017
    Keywords: Missile , autopilot

    Three-loop autopilot of spinning missiles

    Li, Keyong / Yang, Shuxing / Zhao, Liangyu | SAGE Publications | 2014
    Keywords: Spinning missile , three-loop autopilot

    Augmented predictive functional control for missile autopilot design

    Guo, Jianguo / Wang, Guoqing / Guo, Zongyi et al. | SAGE Publications | 2017
    Keywords: missile , autopilot

    Super-twisting integral-sliding-mode guidance law considering autopilot dynamics

    Meng, Kezi / Zhou, Di | SAGE Publications | 2018
    Keywords: missile autopilot , Missile guidance law

    Stability Margin Clearance of Missile Autopilot Using μ Anylysis

    Hou, Zhen-Qian / Liang, Xiao-Geng / Wang, Wen-Zheng et al. | Tema Archive | 2012
    Keywords: Autopilot , missile autopilot

    Multi-model approaches to three-axis missile autopilot design under aerodynamic roll angle uncertainty

    Won, D-Y / Tahk, M-J / Kim, Y-H et al. | SAGE Publications | 2012
    Keywords: three-axis missile autopilot

    Design of three-dimensional nonlinear guidance law with bounded acceleration command

    Du, Runle / Meng, Kezi / Zhou, Di et al. | Elsevier | 2015
    Keywords: Dynamics of missile autopilot

    Design and comparison of autopilots of an air-to-surface antitank missile and its terminal guidance study

    Ada, Celâl / Kural, Ayhan | SAGE Publications | 2014
    Keywords: pitch mathematical model of missile , Missile pitch autopilot

    Three-Point Guidance for Intercepting Weaving Targets

    Ratnoo, Ashwini | AIAA | 2016
    Keywords: Autopilot , Missile Systems

    Robust missile longitudinal autopilot design based on equivalent-input-disturbance and generalized extended state observer approach

    Li, Tong / Zhang, Shifeng / Yang, Huabo et al. | SAGE Publications | 2015
    Keywords: Missile longitudinal autopilot

    Aerodynamic coupling model development and autopilot design for highly manoeuvring skid-to-turn missiles

    Kim, S-H / Kim, Y-S / Lee, Y-I et al. | SAGE Publications | 2012
    Keywords: missile autopilot

    Three-axes predictive control of autopilot for missile

    Ada, Celâl / Kural, Ayhan | Emerald Group Publishing | 2017
    Keywords: Autopilot design , Missile dynamic

    Hybrid Switched Gain-Scheduling Control for Missile Autopilot Design

    Yuan, Chengzhi / Liu, Yang / Wu, Fen et al. | AIAA | 2016
    Keywords: Autopilot , Missile Dynamics , Missile Control

    Impact Angle Constrained Integrated Guidance and Control for Maneuvering Target Interception

    He, Shaoming / Song, Tao / Lin, Defu | AIAA | 2017
    Keywords: Surface to Air Missile , Autopilot , Air to Ground Missile , Missile Dynamics

    Adaptive back-stepping sliding mode guidance laws with autopilot dynamics and acceleration saturation consideration

    Geng, Sheng-Tao / Zhang, Jie / Sun, Jing-Guang | SAGE Publications | 2019
    Keywords: second-order dynamics of missile autopilot

    Generalized extended state observer-based H ∞ control design for a missile longitudinal autopilot

    Dong, Yi / Li, Jian / Li, Tong | SAGE Publications | 2016
    Keywords: missile longitudinal autopilot design

    Intercept Angle Missile Guidance Under Time Varying Acceleration Bounds

    Taub, Ilan / Shima, Tal | AIAA | 2013
    Keywords: Autopilot , Missile Guidance , Ground to Ground Missile

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