Title: Maximum likelihood rocket identifier, Rocket dynamics related project.
Department: Aeronautical engineering, chemical engineering, energy managements
Can be used for: Paper presentations, Aero projects, seminars and study purposes.
This Blog post is a response for a request from an engineering student and aeronautical enthusiast. THe topic for today is also relating to the aeronautical department engineering students because for another few days our team has planned to post most engineering projects relating those subjects. A sensor suite determines location and velocity information relating to a missile threat, which is converted to missile or rocket state estimates. The state estimates are transformed into time-invariant dynamic parameters, unique for each missile type.
Sample from the attached project details: A method for estimating at least one of the type and future location of a missile based on information relating to its sensed present position and velocity comprises the steps of estimating from the sensed data a set of estimated missile parameters including at least one of mass flow rate, thrust, specific impulse, gravity-free burn-out velocity, burn-outtime (time to burn-out of the current stage), and mass at burn-out. The set of estimated parameters is compared with a predetermined database corresponding to at least one of nominal mass flow rate, thrust, specific impulse, gravity-free burn-out velocity, burn-out-time, and mass at burn-out parameters for known missiles, to select the best match to the set of estimated parameters. Parameter reference information sets relating to the mass flow rate, thrust, specific impulse, gravity-free burn-out velocity, burn-out-time, and mass at burn-out parameters of that missile which is the best match are accessed. Using kinematic modeling, the sensed position and velocity, and the parameter reference information set of the best match, the future location of the missile is determined.
Download this aero engineering project
Rocket dynamins details here: http://goo.gl/DwTtJ
Department: Aeronautical engineering, chemical engineering, energy managements
Can be used for: Paper presentations, Aero projects, seminars and study purposes.
This Blog post is a response for a request from an engineering student and aeronautical enthusiast. THe topic for today is also relating to the aeronautical department engineering students because for another few days our team has planned to post most engineering projects relating those subjects. A sensor suite determines location and velocity information relating to a missile threat, which is converted to missile or rocket state estimates. The state estimates are transformed into time-invariant dynamic parameters, unique for each missile type.
Sample from the attached project details: A method for estimating at least one of the type and future location of a missile based on information relating to its sensed present position and velocity comprises the steps of estimating from the sensed data a set of estimated missile parameters including at least one of mass flow rate, thrust, specific impulse, gravity-free burn-out velocity, burn-outtime (time to burn-out of the current stage), and mass at burn-out. The set of estimated parameters is compared with a predetermined database corresponding to at least one of nominal mass flow rate, thrust, specific impulse, gravity-free burn-out velocity, burn-out-time, and mass at burn-out parameters for known missiles, to select the best match to the set of estimated parameters. Parameter reference information sets relating to the mass flow rate, thrust, specific impulse, gravity-free burn-out velocity, burn-out-time, and mass at burn-out parameters of that missile which is the best match are accessed. Using kinematic modeling, the sensed position and velocity, and the parameter reference information set of the best match, the future location of the missile is determined.Download this aero engineering project
Rocket dynamins details here: http://goo.gl/DwTtJ