variable thrust

Brain Emotional Learning Based Intelligent Flight Control for A Variable Thrust Axis Based UAV

变推力轴线无人机的大脑情感学习智能飞行控制

The Design and Implementation of a Variable Thrust Liquid Propellant Rocket Engine Control System

一种大范围变推力液体火箭发动机控制器的设计及实现

Numerical Simulation of Inner Flow Field of a Pintle Injector Variable Thrust Rocket Engine

针栓式变推力火箭发动机内流场数值仿真研究

Firstly, the principle, components and control of variable thrust rocket engine are discussed. Then, the regulating ways and the adoptable technologies of thrust are studied, and the applications in astronavigation are analyzed.

论文首先阐述了变推力火箭发动机的工作原理、组成与控制，研究了推力调节途径和可采用的技术手段，并对它在航天领域的应用进行了分析。

Internal ballistic regulating property of variable thrust pintle SRM

喉栓式变推力固体火箭发动机内弹道调节特性

At present moment, the equations of torpedo motion are based on constant thrust. In order to introduce tangential acceleration into the control of torpedo trajectory, equations with variable thrust have to be established.

目前的鱼雷运动方程是建立在恒推力基础上的，为了将切线加速度引入弹道控制，建立变推力方程是必要的。

Variable Gain Solenoid Valve Control System Used for Hypergolic Bipropellant Variable Thrust Rocket Engine

用于双组元自燃推进剂变推力火箭发动机的可变增益电磁阀控制系统

Analysis on response of pressure in non-coaxial variable thrust pintle motor

非同轴式喉栓变推力发动机压强响应分析

The thrust value is constant and the thrust direction is variable.

发动机推力大小为常值，方向可调。