Coning motion stability of spinning missiles with strapdown seekers

被引：16

作者：

He, S. ^{[1
]}

Lin, D. ^{[1
]}

Wang, J. ^{[1
]}

机构：

[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing, Peoples R China

来源：

AERONAUTICAL JOURNAL | 2016年 / 120卷 / 1232期

基金：

中国国家自然科学基金;

关键词：

Spinning Missile; Coning Motion Stability; Strapdown Seeker; Scaling Factor Error; AUTOPILOT; LIMITS; INSTABILITIES; GUIDANCE; ROCKETS;

D O I：

10.1017/aer.2016.75

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper investigates the problem of coning motion stability of spinning missiles equipped with strapdown seekers. During model derivation, it is found that the scaling factor error between the strapdown seeker and the onboard gyro introduces an undesired parasitic loop in the guidance system and, therefore, results in stability issues. Through stability analysis, a sufficient and necessary condition for the stability of spinning missiles with strapdown seekers is proposed analytically. Theoretical and numerical results reveal that the scaling factor error, spinning rate and navigation ratio play important roles in stable regions of the guidance system. Consequently, autopilot gains must be checked carefully to satisfy the stability conditions.

引用

页码：1566 / 1577

页数：12

共 45 条

[31] Analysis of resonance stability for spinning missile [J].

Jia, Bao ;

Xue, Lin ;

Yan, Xiao-Yong .

Guti Huojian Jishu/Journal of Solid Rocket Technology, 2015, 38 (01) :23-29

[32] Algorithm of Target Motion Prediction for Guidance Process based on Strapdown Inertial Navigation Data [J].

Mukhina, Maryna ;

Filyashkin, Mykola ;

Shevchuk, Dmytro ;

Tymoshenko, Nataliia ;

Prokhorenko, Iryna ;

Okhrimenko, Tetiana ;

Ali, Ismail .

CYBERSECURITY PROVIDING IN INFORMATION AND TELECOMMUNICATION SYSTEMS (CPITS 2020), 2020, 2746 :66-+

[33] Two-Step Adaptive Augmented Unscented Kalman Filter for Roll Angles of Spinning Missiles Based on Magnetometer Measurements [J].

Yan, Xiaolong ;

Chen, Guoguang ;

Tian, Xiaoli .

MEASUREMENT & CONTROL, 2018, 51 (3-4) :73-82

[34] Stability of spinning missile with homing proportional guidance law [J].

Hu, Xiao ;

Yang, Shuxing ;

Xiong, Fenfen ;

Zhang, Guoqing .

AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 71 :546-555

[35] STABILITY CRITERIA FOR STANDING AND SPINNING WAVES IN ANNULAR COMBUSTORS [J].

Ghirardo, Giulio ;

Juniper, Matthew P. ;

Moeck, Jonas P. .

ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 4B, 2015,

[36] Research on dynamic stability of rolling missiles employing direct/aerodynamic force compound control [J].

Bai, Lu ;

Lin, Defu ;

Zheng, Duo ;

Lu, Tianyu .

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2024, 238 (09) :837-855

[37] Numerical Investigation on Nonlinear Stability of a Spinning Missile with One Pair of Canards [J].

Shi, Zhong-Jiao ;

Zhao, Liang-Yu ;

Wang, Wei .

INTERNATIONAL CONFERENCE ON MECHANICS AND CONTROL ENGINEERING (MCE 2015), 2015, :428-432

[38] Platform motion disturbance filtering for strapped-down electronically scanned array seekers with disturbance observer [J].

Muhury, Ankita ;

Sadhu, Smita ;

Ghoshal, Tapan Kumar .

INTERNATIONAL JOURNAL OF DYNAMICS AND CONTROL, 2024, 12 (08) :3005-3016

[39] Effects of rotational motion on dynamic aeroelasticity of flexible spinning missile with large slenderness ratio [J].

Li Heng ;

Ye ZhengYin .

AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 94

[40] A Thin Conducting Liquid Film on a Spinning Disk in the Presence of a Magnetic Field: Dynamics and Stability [J].

Uma, B. ;

Usha, R. .

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2009, 76 (04) :1-14

← 1 2 3 4 5 →