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Old 11-04-2018, 01:57 AM   #1
potjoe
Orbinaut
Support TransX planning - IMFD burning : how to burn in IMFD a transX plan ?

Hi everyone ! I've been a long time reader of this wonderful forum, where I learned almost everything about orbiter. But now, with my little orbinaut experience, I'm stuck with something and it pushes me to write my first message.

I'm trying to do a powered slingshot of Venus, in an Earth-Venus-Mars trip. As I've learned here and there, IMFD (still working on it) isn't efficient in terms of slingshot planning. Though I've already found a window using guess and check in TransX. But here comes a few questions : I don't manage to export my data's from my 'plan" to IMFD, and I really don't understand how to interprate transX plan for each step, in order to use IMFD like a DSKY P30 flight computer and set up the delta velocity program according to transX values. Maybe I'm not reading the correct values, or I missed something.

For instance : on the ground, I would have like to use IMFD to launch, since you can check in real time your Ein. Using the target intercept program, tgt Venus, set Tej and time of encounter according to the transX plan, I have different Rinc and Ein values transX escape plan window and surface launch program.

Again, once in orbit : I've tried to copy the data from the transX escape plan to IMFD in order to do the ejection burn. I've read on the forum many methods, but any of them seem to be working : Copy the total delta-v from the escape plan to the Dvf value in delta velocity program, then set the Tej. according to Time to Pe. from transX. Once burned, I'm off from 15 degrees in S. Maj axis diff. I've also tried to copy each value from the eject plan (prograde, Ch. Plane, outward) to Dvf, dvp and dvf, setting up the Tin to the time to Pe. I beautifully scratched in the Pacific, as IMFD burned straight into the planet.

Last but not least, using the target-intercept program, i finally get on my way to Venus : when i started to plan a MCC, IMFD slingshot program (coupled with Target intercept) gave me 13k Dv to correct my trajectory and perform the sling (and i had to change the Tin at mars from 2 months...)

I've seen on the forum many messages about a combined use of these tools, but I can't find out how to export to IMFD the slingshot attitude. There are tutorials about one or the other, but I didn't find one that described a simultaneous use of IMFD and transX. May anyone help me deal with it ?

Thank you all for your help, have a good weekend.

Potjoe

Edit : adding the scenario file with TransX plan
Attached Files
File Type: scn Circular orbit - Earth-Venus-Mars.scn (9.6 KB, 3 views)

Last edited by potjoe; 11-04-2018 at 06:20 PM. Reason: Adding Scenario File
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Old 11-08-2018, 08:49 PM   #2
BrianJ
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Hello
I can't help much with your main question of transfering TransX flyby data into IMFD, but I thought it worth mentioning that when transfering burn dV parameters between TransX<->IMFD (e.g. Forward, Outward, Pl.Change) you need to invert the sign +/- of the Outward and Pl.Change values. I think that's correct.
Cheers,
Brian
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Old 11-08-2018, 09:42 PM   #4
Marijn
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Quote:
Originally Posted by potjoe View Post
 I beautifully scratched in the Pacific, as IMFD burned straight into the planet.
I think this may happen when the Tej is big. I got into the habit of not hitting the AB button before passing the node just before the burn, usually a quarter orbit or so. If your Tej was bigger at the time of pressing the AB button, you can try pressing the AB at a later time to see if that makes a difference.
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Old 11-08-2018, 10:03 PM   #5
potjoe
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Hi

Thanks for your replies !

@BrianJ Ok I didn't notice that transX is giving for instance an outward velocity, whereas IMFD'Dvi stands for inward. But still, the problem is that in TransX escape plan, you only have a positive prograde dv. If you look at the eject plan (step 2) of the scenario, you'll see that the prograde velocity is negative. I assume that the difference is relative to the reference body used at each steps of the plan : in escape plan, you have a positive prograde Dv relative to earth in order to eject the shjp, but this means that relative to the sun (in the eject plan) you're slowing down, correct me if I'm wrong. I'll give it a try setting the delta velocity program reference to sun and try to input the eject plan variables (inverted or not) instead of the escape plan Delta v value. But still, I cannot use this program correctly combined with the map program, because I don't know the attitude of the slingshot from the transX plan (Inclination and PeD). So even if I set up these variables, I would not be able to "check" with the map program that I'm ejecting/targeting/approaching Venus on a good trajectory.

@bcbarnes Yes I've already seen many times both his beginner guide, the trip to Mars you're mentioning and his tutorial with Dimitri (dgatsoulis) about IMFD. I've performed several trip to Mars using these MFDs and making them working together. But David Courtney's video don't describe a slingshot, it's a Earth Mars trip. As I've said, my problem is specifically the combined use of transX and IMFD while performing a slingshot.

---------- Post added at 10:03 PM ---------- Previous post was at 09:56 PM ----------

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Originally Posted by Marijn View Post
 If your Tej was bigger at the time of pressing the AB button, you can try pressing the AB at a later time to see if that makes a difference.
Thanks for sharing ! We would have done a great Mission Control work you and me I think my mistake is somewhere else, each time I tried I really waited the last moment before activating the autopilot, like 300 seconds before Tej or so... And since it was a huge deltav maneuver, I also divided it into two burns : one orbit before Tej, apply some Dv to reduce the total amount while checking that your Pe MJD is matching with your plan ejection time. Thus it's a good way to cut in two smaller burns a huge one.
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Old 11-08-2018, 10:57 PM   #6
Marijn
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Let's try break it down a bit. The trouble begins with the ejection burn to Venus, right?

What does IMFD's map program look like when you set up this burn in a 2nd MFD slaved to the DV program? It should give you an accurate visual representation of the trajectory. If the trajectory (in blue) doesn't look right, I can imagine the MCC will be expensive.

To use IMFD's map program for this, it's advised to set the following values in IMFD's config file:
LegSize 1
LegsPerFrame 64
AdapTol 4
DateFormat 0
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Old 11-09-2018, 02:15 PM   #7
potjoe
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Sorry for this, I tried to give you the most accurate information.
I already configured IMFD with these parameters.

For the eject burn here is how I proceed : taking note of the Delta v value in transX escape plan, I start Delta velocity program. Here I input as Tej the T. To Pe indicated in TransX, and the Delta v in Dvf field. I can see correctly my trajectory in the map program once shared, but 1) the Pe MJD is far off the value of transX, and 2) once performed, the trajectory shown in transX escape plan with the green line is really off the planed trajectory in yellow. Obviously, it will take me to Venus but not with the good attitude, not with the good PeD, and at the wrong date. Am I proceeding correctly for the moment ?
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Old 11-10-2018, 07:48 AM   #8
Marijn
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In this thread, some odd behavior of IMFD regarding the ejection burn is discussed. Perhaps it contains a hint for your problem: https://www.orbiter-forum.com/showth...t=39984&page=2

To be sure this odd behavior is not your problem, find a real or online stopwatch and time the burn. Check whether an IMFD second has the same duration as a real second. You may be surprised.

To deal with this, set up te burn (using off-axis), quit orbiter, resume the current scenario and do the burn. Check te DV values before burning to see they didn't change upon resuming.

Quote:
Originally Posted by potjoe View Post
 I can see correctly my trajectory in the map program once shared, but 1) the Pe MJD is far off the value of transX, and 2) once performed, the trajectory shown in transX escape plan with the green line is really off the planed trajectory in yellow
2 is probably the result of not solving 1. As long as IMFD Map program tells you something is not right, something is not right. That includes the time of arrival PeT. There is no point proceeding if this value is not what it should be.
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Old 11-16-2018, 10:31 AM   #9
Tommy
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Originally Posted by potjoe View Post
 
Here I input as Tej the T. To Pe indicated in TransX, and the Delta v in Dvf field.



I suspect the problem is here. Tej = Time to Ejection, while T to Pe is the time to Periapsis. This is only true if the ejection point exactly the same as the periapsis of your current parking orbit, which is likely not the not be the case. Set Tej in IMFD to equal the time until burn shown in Trans-X.
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