Abstract
The problem of optimizing the maximum range of a glide guided bomb is studied based on the principle of solving optimal control problems using the Radau pseudo-spectral method. The dynamic model of the guided bomb is nondimensionalized. Combining with the Pontryagin minimum principle, the analytic solution of the optimal control and the first-order necessary condition are derived. The trajectory optimization problem is translated to a nonlinear programming via the Radau pseudo-spectral method. Based on covector mapping principle, an optimality verification method is presented for the numerical solution. Simulation results show that the Radau pseudo-spectral method can provide a highly valuable optimal solution for engineering application. Compared with the conventional maximum lift-to-drag ratio gliding trajectory, the trajectory after optimization can be extended by more than 10%.
| Original language | English |
|---|---|
| Pages (from-to) | 1179-1186 |
| Number of pages | 8 |
| Journal | Binggong Xuebao/Acta Armamentarii |
| Volume | 35 |
| Issue number | 8 |
| DOIs | |
| State | Published - 1 Aug 2014 |
Keywords
- Glide guided bomb
- Ordnance science and technology
- Radau pseudo-spectral method
- Trajectory optimization
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