Research Article
Optimal Ascent Guidance for Air-Breathing Launch Vehicle Based on Optimal Trajectory Correction
Table 2
The simulation results for optimal guidance algorithm.
| | Case | (m) | (m/s) | (deg) | Fuel cost (kg) | Fuel cost (tracking method) (kg) |
| | 1 | −28.20 | 0.136 | 0.20 | 4572.19 | 4574.62 | | 2 | 8.59 | −0.03 | −0.15 | 4583.14 | 4628.39 | | 3 | −15.08 | 0.07 | 0.20 | 4584.74 | 4605.66 | | 4 | 108.16 | 0.47 | −0.23 | 4602.92 | 4776.00 | | 5 | −32.43 | 0.19 | −0.16 | 4601.33 | 4688.94 |
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