Abstract
study considers the problem of impact angle constraint and integrated guidance and control (IGC) law design in an integrated manner for maneuvering target interception without knowing target acceleration. To address this problem, the systematic backstepping technique is adopted in IGC law design, where the convergence of line-of-sight (LOS) rate and impact angle error are regulated by two independent virtual control laws. A new smooth second-order sliding mode (SSOSM) differentiator is developed to estimate the derivatives of the virtual control laws.
| Original language | English |
|---|---|
| Pages (from-to) | 2652-2660 |
| Number of pages | 9 |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 40 |
| Issue number | 10 |
| DOIs | |
| Publication status | Published - 2017 |
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He, S., Song, T., & Lin, D. (2017). Impact angle constrained integrated guidance and control for maneuvering target interception. Journal of Guidance, Control, and Dynamics, 40(10), 2652-2660. https://doi.org/10.2514/1.G002201