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9ca604049e
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Initial 6DoF implementation. The Euler rigid body dynamical equations are present, but there are no torques yet
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2023-04-17 18:53:22 -06:00 |
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23566efa67
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Add terminateCondition to Rocket class. Allows the propagator to check the rocket for a terminate condition instead of hardcoding it in the propagator itself
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2023-04-15 16:50:36 -06:00 |
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a33aeea77a
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Added dynamic thrust computation in Rocket and Propagator
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2023-04-15 14:49:19 -06:00 |
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48d1a933ab
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add a timer to the propagator to record propagation time in runUntilTerminate()
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2023-04-10 20:02:55 -06:00 |
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0734d6a013
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improvements to propagator getForceXYZ methods. The propagator now reaches out to the QtRocket singleton for current gravity data at each timestep. Can easily do the same for atmospheric density next
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2023-04-10 19:19:11 -06:00 |
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b77ba0ef04
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Update the README, so that if anyone stumbles on this repo before it's actually ready for any sort of public release, they should be fairly warned. It might be good to actually just make the repo private before release, but I am not that self-conscious about it
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2023-04-10 18:52:14 -06:00 |
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ed34061195
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removing temporary build artifacts that were accidentally committed
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2023-04-10 18:36:48 -06:00 |
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f595562de9
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refactored MainWindow compute ballistic trajector to use new Rocket interface
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2023-04-09 17:00:37 -06:00 |
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f172e26d01
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Added ConstantGravityModel. Always -9.8 m/s**2 in the z-direction
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2023-04-07 17:08:45 -06:00 |
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90e5289609
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change rk4 integrator to take vector of doubles, spin off Qt gui in separate thread
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2023-04-07 17:08:45 -06:00 |
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1b855b2997
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WIP
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2023-04-07 17:08:45 -06:00 |
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39920e2777
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WIP. Added templated RK4 solver and some more framework code
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2023-04-07 17:08:44 -06:00 |
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6e00f22ce4
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WIP
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2023-04-07 17:08:44 -06:00 |
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8d663f858b
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Added RK4 solver
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2023-04-07 17:08:44 -06:00 |
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92c2986d46
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Change to Qt toolkit and Qt Creator
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2023-04-07 17:08:44 -06:00 |
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