您好,欢迎来到聚文网。 登录 免费注册
战术导弹制导控制系统设计(英文)(第2版)

战术导弹制导控制系统设计(英文)(第2版)

  • 字数: 434
  • 出版社: 北京理工大学
  • 作者: 林德福//何绍溟//李虹言//祁载康|
  • 商品条码: 9787576344646
  • 适读年龄: 12+
  • 版次: 2
  • 开本: 16开
  • 页数: 288
  • 出版年份: 2024
  • 印次: 1
定价:¥62 销售价:登录后查看价格  ¥{{selectedSku?.salePrice}} 
库存: {{selectedSku?.stock}} 库存充足
{{item.title}}:
{{its.name}}
精选
内容简介
本书是《战术导弹制导 控制系统设计》第2版英文 版教材,全面深入地介绍了 战术导弹制导控制系统设计 的相关知识。首先阐述了导 弹制导控制基础,包括概述 与控制方法。接着构建了导 弹数学模型,涵盖符号定义 、刚体运动方程等内容。然 后介绍了基本控制组件数学 模型,如导引头、作动器等 。 书中对制导雷达和导引 头进行了详细分析,涉及雷 达性能影响因素、导引头的 结构、抗干扰机制及各种寄 生回路模型。在自动驾驶仪 设计方面,讲解了多种类型 的自动驾驶仪。此外,还介 绍了视线制导、比例导引及 扩展比例导引等制导律,以 及最优轨迹成型制导方法, 包括最优误差动态分析、预 测-校正制导、重力转弯辅 助制导和三维反舰导弹最优 冲击时间制导等,并给出了 相关的设计、分析及仿真内 容。书末附有参考文献,便 于读者进一步深入研究。
目录
1 Basics of Missile Guidance Control §1.1 Overview §1.2 Missile Control Methods 2 Missile Mathematical Model §2.1 Symbols and Definitions §2.2 Euler Equations of the Missile Rigid Body Motion §2.3 Configuration of the Control Surfaces §2.4 Aerodynamic Derivatives and the Missile Control Dynamic Coefficients §2.5 The Transfer Function of a Missile as the Controlled Object 3 Basic Missile Control Component Mathematical Models §3.1 Seeker §3.2 Actuator §3.3 Gyroscope §3.4 Accelerometer §3.5 Inertial Navigation Components and Integrated Inertial Navigation Module 4 Guidance Radar §4.1 Introduction §4.2 Motion Characteristic of the Target LOS §4.3 Control Loop of the Guidance Radar §4.4 Effect of Receiver Thermal Noise on Guidance Radar Performance §4.5 Effect of Target Glint on Guidance Radar Performance §4.6 Effect of Other Disturbances on Guidance Radar Performance 4.6.1 Effect of Disturbance Moment on Tracking Radar Performance 4.6.2 Effect of Target Maneuvers 5 Seekers §5.1 Overview §5.2 Electromechanical Structure of Commonly Used Seekers 5.2.1 Dynamic Gyro Seeker 5.2.2 Stabilized Platform-based Seeker 5.2.3 Detector Strap-down Stabilized Optic Seeker 5.2.4 Semi-strap-down Platform Seeker 5.2.5 Strap-down Seeker 5.2.6 Roll-pitch Seeker §5.3 Mechanism Analysis of the Anti-disturbance Moment of the Seeker's Stabilization Loop and Tracking Loop §5.4 Transfer Function of Body Motion Coupling and the Parasitic Loop 5.4.1 Transfer Function of Body Motion Coupling 5.4.2 Seeker-missile Coupling Introduced Guidance Parasitic Loop §5.5 A Real Seeker Model and Testing Methods 5.5.1 A Real Seeker Model 5.5.2 Testing Methods for Modeling the Real Seeker §5.6 Other Parasitic Loop Models 5.6.1 Parasitic Loop Model for a Phase Array Strap-down Seeker 5.6.2 Parasitic Loop Due to Radome Slope Error 5.6.3 Beam Control Gain Error ΔK_B of the Phased Array Seeker and the Radome Slope Error R_dom Effect on the Seeker's Performance 5.6.4 A Novel Online Estimation and Compensation Method for Strap-down Phased Array Seeker Disturbance Rejection Effect Using Extended State Kalman Filter §5.7 Stabilization Loop and Tracking Loop Design of the Platform-based Seeker 5.7.1 Stabilization Loop Design 5.7.2 Tracking Loop Design 6 Autopilot Design §6.1 Acceleration Autopilot

蜀ICP备2024047804号

Copyright 版权所有 © jvwen.com 聚文网