Good evening everyone,
I have had Orbiter for a long time, but my attempts at precision long distance spaceflight/ orbital rendezvous have left me somewhat frustrated. I know that a rendezvous MFD currently exists and it uses the Hill equations if the separation is within 700 km.
Now my problems are as follows: First, I have trouble aligning the orbital planes. (the align planes MFD does fine for adjusting inclination, but does little for the Line of Nodes). Second, I have trouble making a Hohman Transfer Orbit such that I can arrive reasonably close to my target (5 or 6 km) so I can close the distance and dock.
My solution is to make MFD's to solve each problem. I have a strong enough background in orbital mechanics and math that figuring out the calculations to solve each problem is not too big of an issue. I also have experience with programming in MATLAB so I am familiar with writing code and debugging etc.
What I am not familiar with is Orbiter MFD devellopment or how its mechanics modeling engine works. I have an algorithm written down for how I would solve both the alignment and rendezvous maneuvers from a conceptual standpoint. That led me to a small issue.
Is ORBITER capable of doing a coordinate transform to work backwards to find the radius and Velocity vector pair in the Geocentric Coordinate system when the orbital elements at that time are known. Second is it possible to make the MFD orient the spacecraft using the direction vector for the burn in 3 dimensional cartesian coordinates, or am I going to have to do another coordinate tranform back to the system used by the Orbit mode on the HUD.
I am sorry for the length of the post. Any help wpuld be appreciated!
I have had Orbiter for a long time, but my attempts at precision long distance spaceflight/ orbital rendezvous have left me somewhat frustrated. I know that a rendezvous MFD currently exists and it uses the Hill equations if the separation is within 700 km.
Now my problems are as follows: First, I have trouble aligning the orbital planes. (the align planes MFD does fine for adjusting inclination, but does little for the Line of Nodes). Second, I have trouble making a Hohman Transfer Orbit such that I can arrive reasonably close to my target (5 or 6 km) so I can close the distance and dock.
My solution is to make MFD's to solve each problem. I have a strong enough background in orbital mechanics and math that figuring out the calculations to solve each problem is not too big of an issue. I also have experience with programming in MATLAB so I am familiar with writing code and debugging etc.
What I am not familiar with is Orbiter MFD devellopment or how its mechanics modeling engine works. I have an algorithm written down for how I would solve both the alignment and rendezvous maneuvers from a conceptual standpoint. That led me to a small issue.
Is ORBITER capable of doing a coordinate transform to work backwards to find the radius and Velocity vector pair in the Geocentric Coordinate system when the orbital elements at that time are known. Second is it possible to make the MFD orient the spacecraft using the direction vector for the burn in 3 dimensional cartesian coordinates, or am I going to have to do another coordinate tranform back to the system used by the Orbit mode on the HUD.
I am sorry for the length of the post. Any help wpuld be appreciated!