Add to ORKGDerivation of three-dimensional three-degree-of- freedom reentry equations of motion in terrestrial navigational coordinate
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
The general solution for the optimum three-dimensional aerodynamic control of a lifting vehicle ente...
The necessity of providing a real-time simulation of controlled reentries of the Gemini vehicle for ...
An inertial navigation system utilizing a servo-controlled two degree of freedom pendulum to obtain ...
Inertial navigation equations are developed which use area navigation (RNAV) waypoints and runway re...
This dissertation presents a method for on-board generation of three-degree-of-freedom (3DOF) constr...
Spacecraft attitude control with strapdown inertial reference system and onboard digital compute
Digital computer program for performance analysis of all inertial guidance system along reference tr...
Navigation is defined as the process of estimating the six degrees of freedom. We have seen an incre...
IBM 7094 computer program for simulating atmospheric entry aided-inertial guidance system
Computer program analyzes the entries and planetary trajectories of space vehicles. It obtains the e...
Computer program for simulating lifting vehicle atmospheric entry flight trajector
Computer programs for simulating booster nominal trajectories for interplanetary mission
During the re-entry phase of a manned satellite, some equipment for continuous on-board indication o...
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
The general solution for the optimum three-dimensional aerodynamic control of a lifting vehicle ente...
The necessity of providing a real-time simulation of controlled reentries of the Gemini vehicle for ...
An inertial navigation system utilizing a servo-controlled two degree of freedom pendulum to obtain ...
Inertial navigation equations are developed which use area navigation (RNAV) waypoints and runway re...
This dissertation presents a method for on-board generation of three-degree-of-freedom (3DOF) constr...
Spacecraft attitude control with strapdown inertial reference system and onboard digital compute
Digital computer program for performance analysis of all inertial guidance system along reference tr...
Navigation is defined as the process of estimating the six degrees of freedom. We have seen an incre...
IBM 7094 computer program for simulating atmospheric entry aided-inertial guidance system
Computer program analyzes the entries and planetary trajectories of space vehicles. It obtains the e...
Computer program for simulating lifting vehicle atmospheric entry flight trajector
Computer programs for simulating booster nominal trajectories for interplanetary mission
During the re-entry phase of a manned satellite, some equipment for continuous on-board indication o...
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
The general solution for the optimum three-dimensional aerodynamic control of a lifting vehicle ente...