This paper presents a high-performance and simple guidance method for a short-range
missile. Missile control systems are designed along the estimated flight envelope of the …

Impact angle is defined as the angle between the velocity vectors of a missile and a target at
the instance of interception. The objective of the impact angle control guidance (IACG) law is …

The design of a rule-based guidance law for homing missiles onto targets is presented. The
stability of the missile-target dynamics is proven. Unlike conventional approaches that solve …

应用模拟导弹制导的方法, 提出了一种考虑系统优化的单车实时动态路径算法.
算法以单车时间最短为目标, 通过使车辆避开拥堵, 达到单车路径规划利于系统优化的目标 …

The traditional approach to improving the lethality of a missile has been to concentrate
efforts in the guidance and control systems to improve accuracy and agility. In this paper, we …

A dynamic and real-time single-vehicle path algorithm considering system optimization is
proposed by the method of simulating missile guidance. Targeted at minimizing the run-time …

In this paper we consider the problem of air to ground missile guidance system using fuzzy
controller which uses Pure Pursuit method. The fuzzy controller's rules are defined using …

This paper presents a high-performance and simple guidance method for a short-range
missile. Missile control systems are designed along the estimated flight envelope of the …

Ten-Koh is a small lean satellite developed by Kyushu Institute of Technology which was
launched in piggyback with GOSAT2 and KhalifaSat on 29thOctober 2018, at 13: 08 Japan …

Within the defence industry, there is the need to provide an improvement in the efficiency
(performance) of a missile system. The present generation of missile systems are sub …