Abstract:

In view of the difference between the present heavy weight airdorp mathematical model and the real system, the model assumption is relaxed and the parachute force direction is presented. The improved heavy eight airdrop model is established which covers many influence factors including rigid body good, angle of cabin floor and parachute. Due to the complexity of the modeling process, the separation body method is improved, which simplifies the modeling process and improves the model extensibility. The model is proved that it has smaller modeling errors and is more realistic compared with the present mathematical model by the simulation result.