Research on Sliding Mode Method about Three-Dimensional Integrated Guidance and Control for Air-to-Ground Missile
Based on adaptive sliding mode-control and back-stepping design method, an integrated guidance and control method with less calculation is proposed, which is designed for air-to-ground missile during the terminal course in three-dimensional space. The model of the control system with nonlinear and c...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Departamento de Ciência e Tecnologia Aeroespacial
2019-01-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: |