Abstract
Based on finite-time H2 performance measure, a criterion of analysis and design is given and a type of optimal maneuver is designed in consideration of both energy cost and miss distance. In the light of an interceptor guidance law with uncertainties, a method of finite-time robust H2 performance analysis and a guaranteed cost control criterion are derived, and the guaranteed performance maneuver is designed under the condition of interceptor guidance law with uncertainty. The results show that a substantial maneuvering near the end of penetration process is most effective, and able to cause large miss distance by minimum energy consumption.
| Original language | English |
|---|---|
| Pages (from-to) | 2289-2294 |
| Number of pages | 6 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 31 |
| Issue number | 10 |
| DOIs | |
| State | Published - Oct 2010 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- Finite-time
- Guaranteed cost control
- H control
- Maneuvering
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