Investigation Of Rocket And Control Systems And Flight Equations OfRocket Motion And The Amount Of Fixed Wing In Low Range Rocket

A rocket is an internal combustion engine (that is, it produces its propulsion power by burning fuel inside theengine) which operates according to Newton's third law (action and reaction). A missile is a device that has a body,a propellant, a warhead, a seeker and a control system. It is a very practical device and produced in high variations.The missiles have three control systems. These systems include wing control, tail control and canard control.Choosing the right arrangement of fixed and moving blocks in a system will create a suitable control command.Combining each of the blocks with another for a missile is also normal and has its own advantages anddisadvantages. The missile in question in this article was small and short range. The missile has a control system ofcanard and tail-stabilizing beam, and in this article, the type analysis including the analysis of the number and angleof the tail-stabilizing blade has been investigated. At first, explanations about the rocket, flight equations and thensimulations have been made. And finally, a detailed analysis of the layout is provided.

کلیدواژه ها:

Control system ، control beam ، stabilizer beam ، missile ، flight equations