Add to ORKGA study is made of the families of non-thrusting ascent trajectories during rendezvous with an orbiting space station and the descent trajectories to the earth's atmosphere. Equations of motion are derived and results are shown for two typical orbits of the station (one circular and one elliptic orbit}. Boundaries of launch (at time of booster burnout) and rendezvous conditions are given and the effects of delays in launch time are discussed
The accomplishment of orbital rendezvous maneuvers involves a very complex and risky process, especi...
An analytical and simulation study was conducted of an automatic system to control the terminal phas...
The rendezvous of a pilot-controlled space ferry vehicle with an orbiting space station was simulate...
A study is made of the families of non-thrusting ascent trajectories of a ferry vehicle during rende...
A digital-computer simulation was made of the midcourse or ascent phase of a rendezvous between a fe...
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 ...
Collision and pursuit course closure maneuvers were studied for correcting position and velocity err...
Simulated docking maneuvers were performed to assess the effect of initial velocity on docking failu...
When launching a spacecraft from Earth parking orbit to deep space, it is highly desirable to have t...
summary:The rendezvous realised by the cotangential transfer between two prescribed flightpaths is s...
An experiment was performed in the Space Station Proximity Operations Simulator at the NASA Ames Res...
Effect of using two separate engines in lunar lander for direct-return rendezvous with vehicl
Flight scheduling in planar two burn minimum fuel rendezvous of interceptor with target vehicle
Active rendezvous of an unmanned spacecraft with the Space Transportation System (STS) Shuttle is co...
The accomplishment of orbital rendezvous maneuvers involves a very complex and risky process, especi...
An analytical and simulation study was conducted of an automatic system to control the terminal phas...
The rendezvous of a pilot-controlled space ferry vehicle with an orbiting space station was simulate...
A study is made of the families of non-thrusting ascent trajectories of a ferry vehicle during rende...
A digital-computer simulation was made of the midcourse or ascent phase of a rendezvous between a fe...
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 ...
Collision and pursuit course closure maneuvers were studied for correcting position and velocity err...
Simulated docking maneuvers were performed to assess the effect of initial velocity on docking failu...
When launching a spacecraft from Earth parking orbit to deep space, it is highly desirable to have t...
summary:The rendezvous realised by the cotangential transfer between two prescribed flightpaths is s...
An experiment was performed in the Space Station Proximity Operations Simulator at the NASA Ames Res...
Effect of using two separate engines in lunar lander for direct-return rendezvous with vehicl
Flight scheduling in planar two burn minimum fuel rendezvous of interceptor with target vehicle
Active rendezvous of an unmanned spacecraft with the Space Transportation System (STS) Shuttle is co...
The accomplishment of orbital rendezvous maneuvers involves a very complex and risky process, especi...
An analytical and simulation study was conducted of an automatic system to control the terminal phas...
The rendezvous of a pilot-controlled space ferry vehicle with an orbiting space station was simulate...