Topics
fighterAircraft
A general procedure for computing the region of influence of a maneuvering vehicle is described. Basic differential geometric relations, including the use of a general trajectory parameter and the introduction of auxiliary variables in the envelope theory are presented. To illustrate the application of the method, the destruct region for a maneuvering fighter firing missiles is computed
Optimal control processes in systems with distributed parameters, and problems of invariance theor
One geometry currently under consideration for the Aeroassist Flight Experiment (AFE) vehicle is com...
The primary objective is to determine how an airplane configuration should be modeled to predict bot...
Slender body methods were applied to some specialized problems associated with missile configuration...
May 1986Also issued as an M.S. thesis, Massachusetts Institute of Technology. Dept. of Aeronautics a...
A computer technique to determine the mission radius and maneuverability characteristics of combat a...
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...
AbstractThe evasive boundaries of two types of fighters which have different g performances, against...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77380/1/AIAA-1998-4547-770.pd
Nowadays, the homing guidance is utilized in the existed and under development air defense systems (...
Approximation method for solving singe-degree-of- freedom differential roll equation with time depen...
The emergence of current high-interest mission involving aeromaneuvering hypersonic flight has given...
Intercept geometry of target aircraft and missiles play an important role in determining the effect...
The problem of determining the geometry of non-slender axisymmetric missile of minimum ballistic fac...
Optimal control processes in systems with distributed parameters, and problems of invariance theor
One geometry currently under consideration for the Aeroassist Flight Experiment (AFE) vehicle is com...
The primary objective is to determine how an airplane configuration should be modeled to predict bot...
Slender body methods were applied to some specialized problems associated with missile configuration...
May 1986Also issued as an M.S. thesis, Massachusetts Institute of Technology. Dept. of Aeronautics a...
A computer technique to determine the mission radius and maneuverability characteristics of combat a...
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...
AbstractThe evasive boundaries of two types of fighters which have different g performances, against...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77380/1/AIAA-1998-4547-770.pd
Nowadays, the homing guidance is utilized in the existed and under development air defense systems (...
Approximation method for solving singe-degree-of- freedom differential roll equation with time depen...
The emergence of current high-interest mission involving aeromaneuvering hypersonic flight has given...
Intercept geometry of target aircraft and missiles play an important role in determining the effect...
The problem of determining the geometry of non-slender axisymmetric missile of minimum ballistic fac...
Optimal control processes in systems with distributed parameters, and problems of invariance theor
One geometry currently under consideration for the Aeroassist Flight Experiment (AFE) vehicle is com...
The primary objective is to determine how an airplane configuration should be modeled to predict bot...
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