Apogee Prediction on Real Flight Evaluation Data 1.0 (test)
315.6Apogee (m)OpenRocket baseline
Evaluation results
| Method | Links | ||||
|---|---|---|---|---|---|
| OpenRocket baselineMotor=F24-4W, Configuration (Cfg)=A, Flight ID=22025.12 | 315.6 | — | — | — | |
| OpenRocket baselineMotor=F24-4W, Configuration (Cfg)=A, Flight ID=32025.12 | 315.6 | — | — | — | |
| OpenRocket baselineMotor=F24-4W, Configuration (Cfg)=A, Flight ID=92025.12 | 315.6 | — | — | — | |
| amortized inference approachMotor=F24-4W, Configuration (Cfg)=A, Flight ID=2, Inferred Drag Coefficient (Cd_hat)=0.845, Inferred Thrust Factor (alpha_hat)=0.8362025.12 | 286.3 | — | — | 5 | |
| amortized inference approachMotor=F24-4W, Configuration (Cfg)=A, Flight ID=3, Inferred Drag Coefficient (Cd_hat)=0.888, Inferred Thrust Factor (alpha_hat)=0.7832025.12 | 263.6 | — | — | 17 | |
| amortized inference approachMotor=F24-4W, Configuration (Cfg)=A, Flight ID=9, Inferred Drag Coefficient (Cd_hat)=0.894, Inferred Thrust Factor (alpha_hat)=0.7762025.12 | 260.5 | — | — | 19.1 | |
| OpenRocket baselineMotor=F39, Configuration (Cfg)=B, Flight ID=102025.12 | 226.5 | — | — | — | |
| OpenRocket baselineMotor=F39, Configuration (Cfg)=B, Flight ID=112025.12 | 226.5 | — | — | — | |
| OpenRocket baselineMotor=F39, Configuration (Cfg)=B, Flight ID=122025.12 | 226.5 | — | — | — | |
| OpenRocket baselineMotor=E35-5W, Configuration (Cfg)=A, Flight ID=42025.12 | 218.4 | — | — | — | |
| amortized inference approachMotor=F39, Configuration (Cfg)=B, Flight ID=12, Inferred Drag Coefficient (Cd_hat)=0.876, Inferred Thrust Factor (alpha_hat)=0.7842025.12 | 212.6 | — | — | 14.5 | |
| amortized inference approachMotor=F39, Configuration (Cfg)=B, Flight ID=11, Inferred Drag Coefficient (Cd_hat)=0.878, Inferred Thrust Factor (alpha_hat)=0.7822025.12 | 211.7 | — | — | 15.4 | |
| amortized inference approachMotor=F39, Configuration (Cfg)=B, Flight ID=10, Inferred Drag Coefficient (Cd_hat)=0.890, Inferred Thrust Factor (alpha_hat)=0.7682025.12 | 206.2 | — | — | 20.3 | |
| OpenRocket baselineMotor=E35-5W, Configuration (Cfg)=B, Flight ID=12025.12 | 198.2 | — | — | — | |
| amortized inference approachMotor=E35-5W, Configuration (Cfg)=A, Flight ID=4, Inferred Drag Coefficient (Cd_hat)=0.838, Inferred Thrust Factor (alpha_hat)=0.8222025.12 | 180.9 | — | — | 6.2 | |
| amortized inference approachMotor=E35-5W, Configuration (Cfg)=B, Flight ID=1, Inferred Drag Coefficient (Cd_hat)=0.659, Inferred Thrust Factor (alpha_hat)=0.8872025.12 | 170.8 | — | — | 1 | |
| amortized inference approachsubset=Valid flights (8)2025.12 | — | 12.3 | 14 | — | |
| OpenRocket baselinesubset=Valid flights (8)2025.12 | — | 19.9 | 23.1 | — |