咨询与建议

限定检索结果

文献类型

  • 28 篇 期刊文献
  • 1 篇 会议

馆藏范围

  • 29 篇 电子文献
  • 0 种 纸本馆藏

日期分布

学科分类号

  • 26 篇 工学
    • 22 篇 航空宇航科学与技...
    • 21 篇 仪器科学与技术
    • 4 篇 控制科学与工程
    • 1 篇 力学(可授工学、理...
    • 1 篇 机械工程
  • 21 篇 管理学
    • 21 篇 管理科学与工程(可...
  • 4 篇 理学
    • 4 篇 数学

主题

  • 29 篇 linear quadratic...
  • 9 篇 guidance laws
  • 8 篇 proportional nav...
  • 7 篇 flight path angl...
  • 6 篇 riccati equation...
  • 5 篇 autopilot
  • 4 篇 linear quadratic...
  • 3 篇 matlab
  • 3 篇 heading angle
  • 3 篇 feedback control
  • 3 篇 numerical simula...
  • 3 篇 homing missile
  • 3 篇 computing
  • 2 篇 closed loop tran...
  • 2 篇 guidance system
  • 2 篇 white noise
  • 2 篇 terminal sliding...
  • 2 篇 state space repr...
  • 2 篇 homing guidance
  • 2 篇 kalman filter

机构

  • 2 篇 indian inst sci ...
  • 1 篇 chepstow wales n...
  • 1 篇 mechanical engin...
  • 1 篇 kyushu univ dept...
  • 1 篇 shandong univ de...
  • 1 篇 usn ctr surface ...
  • 1 篇 southern univ sc...
  • 1 篇 natl acad sci uk...
  • 1 篇 general electric...
  • 1 篇 university of ca...
  • 1 篇 univ colorado ae...
  • 1 篇 baku state univ ...
  • 1 篇 n carolina state...
  • 1 篇 delft university...
  • 1 篇 beihang univ sch...
  • 1 篇 cambridge res co...
  • 1 篇 fudan univ dept ...
  • 1 篇 cabinet d'etudes...
  • 1 篇 rutgers state un...
  • 1 篇 univ missouri de...

作者

  • 2 篇 shima tal
  • 1 篇 curtain rf
  • 1 篇 markham keith c.
  • 1 篇 lin cf
  • 1 篇 mingori dl
  • 1 篇 speyer jl
  • 1 篇 gajic z
  • 1 篇 scheeres daniel ...
  • 1 篇 bando mai
  • 1 篇 ghose debasish
  • 1 篇 xin ming
  • 1 篇 ratnoo ashwini
  • 1 篇 fabbri g.
  • 1 篇 goldys b.
  • 1 篇 longman rw
  • 1 篇 ohlmeyer e. j.
  • 1 篇 mcreynolds sr
  • 1 篇 tekin raziye
  • 1 篇 tahk min-jea
  • 1 篇 sun zhongyang

语言

  • 28 篇 英文
  • 1 篇 其他
检索条件"主题词=Linear Quadratic Control Problem"
29 条 记 录,以下是21-30 订阅
排序:
A linear-quadratic OPTIMAL-control problem WITH DISTURBANCES - AN ALGEBRAIC RICCATI EQUATION AND DIFFERENTIAL-GAMES APPROACH
收藏 引用
APPLIED MATHEMATICS AND OPTIMIZATION 1994年 第3期30卷 267-305页
作者: CHEN, SP LI, XJ PENG, SG YONG, JM FUDAN UNIV DEPT MATHSHANGHAIPEOPLES R CHINA SHANDONG UNIV DEPT MATHJINANPEOPLES R CHINA
A linear quadratic optimal control problem with coexisting initial and persistent disturbances is studied. Upper and lower values and relevant algebraic Riccati equations (ARE for short) are introduced. Various relati... 详细信息
来源: 评论
ANALYTIC SOLUTION OF THE RICCATI EQUATION FOR THE HOMING MISSILE linear-quadratic control problem
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1994年 第3期17卷 619-621页
作者: LOVREN, N TOMIC, M UNIV SARAJEVO FAC MECH ENGNDEPT MATH71000 SARAJEVOBOSNIA & HERCEG
This Note has presented the analytic derivation of the optimal closed-loop guidance law for a finite-bandwidth homing missile intercepting a maneuvering target and has provided a simple analytic means of solving the m... 详细信息
来源: 评论
Periodic optimal flight
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1996年 第4期19卷 745-755页
作者: Speyer, JL University of California Los Angeles Los Angeles California 90024-1597
For a host of dynamic systems, periodic motion is more efficient than steady-state operation. This work focuses on atmospheric fuel-efficient periodic flight. To understand some of the generic properties of periodic o... 详细信息
来源: 评论
FREQUENCY-WEIGHTED SYSTEM-IDENTIFICATION AND linear quadratic controlLER-DESIGN
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1993年 第2期16卷 330-336页
作者: HORTA, LG PHAN, M JUANG, JN LONGMAN, RW SULLA, JL LOCKHEED ENGN & SCI CO HAMPTONVA 23666
Application of filters for the frequency weighting of Markov parameters (pulse response functions) is described in relation to system/observer identification. The time domain identification approach recovers a model t... 详细信息
来源: 评论
FIXED-INTERVAL SMOOTHING - REVISITED
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1990年 第5期13卷 913-921页
作者: MCREYNOLDS, SR General Electric Company Philadelphia Pennsylvania 19101
Gaps in the derivation of early fixed-interval smoothers are filled in. Particular attention is paid to the use of the yariational approach introduced by Bryson and Frazier. The notion of complementary models introduc... 详细信息
来源: 评论
A SIMPLE ALGORITHM FOR THE SELECTION OF TERMINAL PENALTY WEIGHTING MATRICES
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1986年 第4期9卷 503-505页
作者: CHUN, HM TURNER, JD CAMBRIDGE RES CONTROL THEORY DYNAM GRPCAMBRIDGEMA
A simple iterative algorithm has been presented for selecting terminal penalty weighting matrices for linear-quadratic control problems. The algorithm selects a weighting matrix which yields acceptable system performa... 详细信息
来源: 评论
COMPARISON OF ANGULAR AND METRIC GUIDANCE LAWS FOR TACTICAL MISSILES
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1986年 第4期9卷 505-507页
作者: DURIEUX, JL Cabinet d'Etudes Techniques d'Automatisation Angouleme France
The laws describing modern guidance systems are based on the methods of optimal control. This note compares an angular guidance law optimized by the adjoint technique and a metric law comprising an optimal estimator c... 详细信息
来源: 评论
USE OF FREQUENCY-DEPENDENCE IN linear quadratic control-problemS TO FREQUENCY-SHAPE ROBUSTNESS
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1985年 第3期8卷 397-401页
作者: ANDERSON, BDO MINGORI, DL UNIV CALIF LOS ANGELES DEPT MECH AEROSP & NUCL ENGNLOS ANGELESCA 90024
linear quadratic control problems are considered where frequency-dependent weighting on the control is assumed. When high frequencies are weighted more heavily than low frequencies, two qualitative conclusions can be ... 详细信息
来源: 评论
ROBUST MISSILE AUTOPILOT DESIGN USING A GENERALIZED SINGULAR OPTIMAL-control TECHNIQUE
收藏 引用
JOURNAL OF GUIDANCE control AND DYNAMICS 1985年 第4期8卷 498-507页
作者: LIN, CF LEE, SP LITTON GUIDANCE & CONTROL LAND VEHICLE SYST WOODLAND HILLSCA
A generalized singular linear quadratic control technique is developed to design an optimal trajectory tracking system. The output feedback control law is designed using this technique. The feedback gain matrix is syn... 详细信息
来源: 评论