Add to ORKGResults of a study to optimize the guidance gains for the analytical drag control entry guidance system are presented. The guidance gains were optimized for study points chosen in all phases of entry
Research data covering orbit determination, optimization techniques, and trajectory design for manne...
A nonlinear six degree of freedom entry simulation study was conducted to identify space shuttle gui...
Assessment of disturbance torques due to interaction of spacecraft with atmosphere in long duration ...
The Analytic Drag Control (ADC) entry guidance has been developed and baselined for the space shuttl...
During planetary entry, a vehicle uses drag generated from flight through the planetary atmosphere t...
The derivations of mathematical models in Vol. 1 are presented along with descriptions of all periph...
The steering system of the space shuttle vehicle is presented for the several hundred miles of fligh...
The Space Shuttle descent mission planning, mission design, deorbit targeting, and entry guidance ha...
The practical application of real-time performance optimization is addressed (using a wide-body tran...
A summary of the aerodynamic characteristics of the delta orbiter space shuttle vehicle is presented...
The optimization technique is described which was used in the study for applying modern optimal cont...
This note shows that a feasible reference drag profile for the first entry portion of a skip entry c...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
The selection of a trim solution that provides the space shuttle with the highest level of performan...
The results of a study to analyze, design, and evaluate guidance and control systems are presented ...
Research data covering orbit determination, optimization techniques, and trajectory design for manne...
A nonlinear six degree of freedom entry simulation study was conducted to identify space shuttle gui...
Assessment of disturbance torques due to interaction of spacecraft with atmosphere in long duration ...
The Analytic Drag Control (ADC) entry guidance has been developed and baselined for the space shuttl...
During planetary entry, a vehicle uses drag generated from flight through the planetary atmosphere t...
The derivations of mathematical models in Vol. 1 are presented along with descriptions of all periph...
The steering system of the space shuttle vehicle is presented for the several hundred miles of fligh...
The Space Shuttle descent mission planning, mission design, deorbit targeting, and entry guidance ha...
The practical application of real-time performance optimization is addressed (using a wide-body tran...
A summary of the aerodynamic characteristics of the delta orbiter space shuttle vehicle is presented...
The optimization technique is described which was used in the study for applying modern optimal cont...
This note shows that a feasible reference drag profile for the first entry portion of a skip entry c...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
The selection of a trim solution that provides the space shuttle with the highest level of performan...
The results of a study to analyze, design, and evaluate guidance and control systems are presented ...
Research data covering orbit determination, optimization techniques, and trajectory design for manne...
A nonlinear six degree of freedom entry simulation study was conducted to identify space shuttle gui...
Assessment of disturbance torques due to interaction of spacecraft with atmosphere in long duration ...