This paper uses the data provided by the STK analysis module, makes the simulation design of spacecraft orbit transferring, and provides data to support the ...
This paper uses the data provided by the STK analysis module, makes the simulation design of spacecraft orbit transferring, and provides data to support the ...
Yi Tan, Yang Wang, Lei Wang, Jiaze Sun: Simulation research on the aircraft orbit transferring based on dragging force using STK. EMEIT 2011: 3863-3866.
This paper discusses the use of solely aerodynamic drag force to perform this targeting, which is especially useful for smaller spacecraft that do not contain ...
Missing: aircraft transferring
Real time three-dimensional simulation platform for satellite mission analysis · Simulation research on the aircraft orbit transferring based on dragging force ...
While orbital drag is an important effect that will act on a spacecraft, the typical assumption is that the satellite will generally remain on orbit. Once the ...
Missing: aircraft | Show results with:aircraft
STK and Java Simulator models of two 1.5U CubeSats initially in identical 600km circular orbits. • One satellite in max drag configuration, other in min drag.
Missing: aircraft | Show results with:aircraft
In this paper, a Model Predictive Control (MPC) approach is applied to spacecraft rendezvous and proximity maneuvering problems in the orbital plane. We ...
Abstract. Low Earth Orbit satellite(LEO) missions have potentially attractive features such as low launch cost, and wide remote sensing applications.
directly using the STK propagator or any other high fidelity simulation environment. ... component which uses a high fidelity numerical orbit simulation to ...
Missing: aircraft | Show results with:aircraft