A mathematical model is developed for an anti-tank missile and its guidance algorithms. The aerodynamic model is separated into two parts, the airframe and external lifting surfaces in order to model damage to the airframe. Radar data is compared to that of the proposed model and it is shown that the model accurately replicates the true flight dynamics. Two types of field handling damage are modeled, a damaged mid-body wing with 50% of its planform area missing, and an un-deployed mid-body wing. Monte Carlo simulations are performed for each type of damage and the eight possible mid-body wing locations. The results predict that the anti-tank guided missile\u27s performance in response to damage is extremely sensitive to the radial location ...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
An anti-tank guided missile is a weapon system primarily designed to hit and destroy armored tanks a...
The purpose of this effort is to create an analytical physics based aircraft-MANPADS model capabilit...
This thesis presents the development of a six-degree-of-freedom flight simulation environment for mi...
This thesis presents the development of a six-degree-of-freedom flight simulation environment for mi...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
Significant research over the years has aimed to redefine the flight capabilities of aircraft after ...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
An anti-tank guided missile is a weapon system primarily designed to hit and destroy armored tanks a...
The purpose of this effort is to create an analytical physics based aircraft-MANPADS model capabilit...
This thesis presents the development of a six-degree-of-freedom flight simulation environment for mi...
This thesis presents the development of a six-degree-of-freedom flight simulation environment for mi...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
A computer-based mathematical model is developed for the estimation of assessment of damage inflict...
Significant research over the years has aimed to redefine the flight capabilities of aircraft after ...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
The authors earlier model for the vulnerability of aircraft where aircraft was considered as a comb...
An anti-tank guided missile is a weapon system primarily designed to hit and destroy armored tanks a...
The purpose of this effort is to create an analytical physics based aircraft-MANPADS model capabilit...