Add to ORKGApproximation method for solving singe-degree-of- freedom differential roll equation with time dependent coefficient - ballistic trajectory anallysi
Study compares the use of five different methods for the computer solution of the restricted three-b...
A general procedure for computing the region of influence of a maneuvering vehicle is described. Bas...
Calculating small rocket trajectories using rocket to launcher radial velocity dat
Perturbation method of trajectory optimization by fast time repetitive computations of state equatio...
Numerical method for rocket trajectory determination from multistation Doppler tracking dat
Theoretical prediction of rolling motion of Nike-Cajun and Nike-Apache rocket vehicle
A time accurate approximate factorization (AF) algorithm is formulated for solution of the three dim...
Calculating rocket vertical flight performance using Newtons law to compute acceleratio
Comparison of fourth order Runge-Kutta numerical integration technique with two numerical integratio...
An extension of the time vector technique for determining stability and control derivatives from fli...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
A predictive method of nonlinear system analysis is used to investigate airplane stability and dynam...
Recursive computation of coefficients for time dependent f and g series solution to two-body problem...
A computational procedure is described which numerically integrates the equations of motion of an un...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77025/1/AIAA-1991-590-705.pd
Study compares the use of five different methods for the computer solution of the restricted three-b...
A general procedure for computing the region of influence of a maneuvering vehicle is described. Bas...
Calculating small rocket trajectories using rocket to launcher radial velocity dat
Perturbation method of trajectory optimization by fast time repetitive computations of state equatio...
Numerical method for rocket trajectory determination from multistation Doppler tracking dat
Theoretical prediction of rolling motion of Nike-Cajun and Nike-Apache rocket vehicle
A time accurate approximate factorization (AF) algorithm is formulated for solution of the three dim...
Calculating rocket vertical flight performance using Newtons law to compute acceleratio
Comparison of fourth order Runge-Kutta numerical integration technique with two numerical integratio...
An extension of the time vector technique for determining stability and control derivatives from fli...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
A predictive method of nonlinear system analysis is used to investigate airplane stability and dynam...
Recursive computation of coefficients for time dependent f and g series solution to two-body problem...
A computational procedure is described which numerically integrates the equations of motion of an un...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77025/1/AIAA-1991-590-705.pd
Study compares the use of five different methods for the computer solution of the restricted three-b...
A general procedure for computing the region of influence of a maneuvering vehicle is described. Bas...
Calculating small rocket trajectories using rocket to launcher radial velocity dat