Add to ORKGDigital computer program SWITCH for trajectory optimization of multiple-burn vacuum rocket flight
Simplified and accurate relative equations of motion for two impulse orbital rendezvou
The compability of the nominal rendezvous sequence with low target orbits is addressed. It was found...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
Program determines if rendezvous in near space is possible, and performs an analysis to determine th...
Computational method for time optimal space rendezvous between rocket vehicle and circular orbit tar...
An analytical and simulation study was conducted of an automatic system to control the terminal phas...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
The current planning process for space shuttle rendezvous with a second Earth-orbiting vehicle is ti...
Closed-form solutions are presented for a two-burn orbit insertion, AOA, and ATO maneuver targets, a...
In recent years, there has been a growing demand for the autonomous rendezvous and docking capabilit...
An investigation of a two-impulse plan for performing rendezvous on a once-a-day basis with a near-e...
A digital-computer simulation was made of the midcourse or ascent phase of a rendezvous between a fe...
A FORTRAN computer program was developed which automatically targets two and three burn rendezvous m...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
Digital computer program SWITCH for trajectory optimization of multiple-burn vacuum rocket flight
Simplified and accurate relative equations of motion for two impulse orbital rendezvou
The compability of the nominal rendezvous sequence with low target orbits is addressed. It was found...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
Program determines if rendezvous in near space is possible, and performs an analysis to determine th...
Computational method for time optimal space rendezvous between rocket vehicle and circular orbit tar...
An analytical and simulation study was conducted of an automatic system to control the terminal phas...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
The current planning process for space shuttle rendezvous with a second Earth-orbiting vehicle is ti...
Closed-form solutions are presented for a two-burn orbit insertion, AOA, and ATO maneuver targets, a...
In recent years, there has been a growing demand for the autonomous rendezvous and docking capabilit...
An investigation of a two-impulse plan for performing rendezvous on a once-a-day basis with a near-e...
A digital-computer simulation was made of the midcourse or ascent phase of a rendezvous between a fe...
A FORTRAN computer program was developed which automatically targets two and three burn rendezvous m...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
Digital computer program SWITCH for trajectory optimization of multiple-burn vacuum rocket flight
Simplified and accurate relative equations of motion for two impulse orbital rendezvou
The compability of the nominal rendezvous sequence with low target orbits is addressed. It was found...