- +(91) 4023006097 ,
- +(91) 4035944424
- +(91) 7989111457
- ask@adyahaways.in
- Mon - Sat 8:00 - 21:00, Sunday - CLOSED
In this research our main agenda is to study the misdistance at the time of missile separation from the aircraft in dynamic motion and recording of history of trajectories at different time interval. The miss-distance can be determined by the shock wave amplitude, while the determination of angular position can be obtained from the hit order between the different pressure sensors located in the missile nose along with miss distance indicator. However, the miss distance and the angular position of the missile trajectories was measured in real time analysis and the data was stored as raw data. Those raw data was compared with the actual test data provided by our client and agreed well with less than 1 % errors.
We are highly productive & versatile for any kind of moving body or 6-DOF motion including writing of 6-DOF & UDF code. An efficient framework has been developed and proposed for 6DOF missile design and simulation. Dynamic grid adaptation techniques were introduced to ensure the convergence of significant constraints to high-fidelity results to increase the reliability and robustness of the optimal configuration at the conceptual design stage without any appreciable turnaround time. The proposed framework has been developed to demonstrate the efficiency and feasibility from the missile conceptual design stage to accurate missile trajectory prediction to meet the requirements reliably and robustly.
