Research on Penetration Technology of Intelligent Cluster Missile System

2019 ◽  
Author(s):  
Zongang Liu ◽  
Jiaguo Lu ◽  
Zhen Dong
Keyword(s):  
Missile System

DESCRIPTION MODEL OF PROSPECTIVELY SIMULATOR OPERATIONAL-TACTICAL MISSILE SYSTEM

2017 ◽  
Vol 62 ◽  
pp. 49-57
Author(s):  
V. V. Belov ◽  
◽  
N. N Vlasov ◽  
D. A. Vodichenkov ◽  
◽  
...  
Keyword(s):  
Missile System

Suboptimal mid-course guidance algorithm for accelerating missiles

2016 ◽  
Vol 231 (11) ◽  
pp. 2032-2047 ◽  
Author(s):  
Min-Guk Seo ◽  
Min-Jea Tahk
Keyword(s):  
Performance Enhancement ◽  
Feedback Form ◽  
Velocity Change ◽  
Guidance Law ◽  
Burn Out ◽  
Homing Performance ◽  
Guidance Algorithm ◽  
Midcourse Guidance ◽  
Missile System ◽  
Loop Form

This paper deals with the closed-loop form of mid-course guidance law design for accelerating missile system, whose acceleration is approximately constant. A midcourse guidance algorithm of feedback form is proposed to satisfy the engagement geometry conditions at the burn-out time for terminal homing performance enhancement. The effect of velocity change due to missile acceleration is explicitly considered in the derivation of the guidance law. The terminal constraint update algorithm is proposed under the assumption that the target trajectory is predicted precisely. Simulation results are provided to show the performance and characteristics of the proposed algorithm.

Research on the New Missile Actuation System with Dual Independent Closed-Loop

2014 ◽  
Vol 551 ◽  
pp. 337-343
Author(s):  
Hui Chen ◽  
Yong Ling Fu ◽  
Juan Chen ◽  
He Song Liu
Keyword(s):  
High Performance ◽  
Closed Loop ◽  
Dynamic Performance ◽  
Actuation System ◽  
High Penetration ◽  
Low Energy Consumption ◽  
Penetration Ability ◽  
Important Direction ◽  
And Performance ◽  
Missile System

With the development of the advanced precision-guided missile and anti-missile system, high precision, high penetration ability and Low energy consumption have become an important direction for the missile. A new missile electro-hydraulic actuation system with dual independent closed-loop is put forward with the trend of high performance and energy-saving, and then the operating principle and process are discussed. Finally the accurate mathematical model is established, and the influence of the different basic pressure on the dynamic performance is analyzed. The simulation results show that the new proposed scheme has made great improvements in reducing the zero-control current of the system, but the efficiency and performance of the actuation system should be considered integrated due to the decrease of the dynamic performance, so it is practical for the future development of the missile electro-hydraulic actuation system.

scholarly journals Algorithm for calculating the covariance matrix of the noise jammer estimated position

2019 ◽  
pp. 43-49
Author(s):  
I. O. Devyatyarov ◽  
V. A. Dobrozhanskiy
Keyword(s):  
Covariance Matrix ◽  
Linear Estimate ◽  
True Position ◽  
Missile System

The study considers an algorithm for identifying the noise jammers tracks and estimates the coordinates of the assumed position of such a jammer as a linear estimate of the true position with minimal dispersion. An algorithm for calculating the covariance matrix of the resulting estimate is proposed. Findings of the research can be used to modify and develop algorithms which ensure the operation of a promising anti-aircraft missile system for noise jamming.

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