Abstract
In this paper, a guidance scheme for impact angle control against maneuvering targets with unknown target acceleration is proposed. In this scheme, the unknown target acceleration is estimated via a linear extended state observer; a novel time-varying global slide mode control technique is presented to eliminate the reaching phase and enforce a desired impact angle exactly at the time of interception with finite-time convergence, good robustness, high precision and smooth guidance command. Moreover, feasible guidance logics are developed to achieve all-aspect interception with the tolerance of large initial heading errors. Numerical simulations in various scenarios are performed to verify the performance of the proposed guidance scheme.
| Original language | English |
|---|---|
| Pages (from-to) | 9192-9208 |
| Number of pages | 17 |
| Journal | Journal of the Franklin Institute |
| Volume | 355 |
| Issue number | 18 |
| DOIs | |
| Publication status | Published - Dec 2018 |
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