Abstract
The traditional integrated guidance and control method can't ensure that the line-of-sight (LOS) satisfies the field-of-view angle constraint of the strap-down seeker. In view of this problem, a new integrated guidance and control method for a strap-down missile considering body field-of-view (FOV) angle constraints is proposed by combining the strap-down decoupling principle and state constraint control method in this paper. Firstly, the integrated guidance and control model considering the FOV constraint is built by employing the strap-down decoupling method, based on which the strict feedback state equation model is derived; secondly, a novel adaptive law for estimating the square of the disturbance bound is designed; thirdly, the FOV constraint issue is handled based on the integral Barrier Lyapunov function and the dynamic surface control. At last, the stability of the closed system and the uniform ultimately boundedness of the signals are proved by the Lyapunov theorem. The numerical simulations imply the effectiveness of the proposed method.
| Translated title of the contribution | Integrated Guidance and Control for A Strap-down Missile Considering Body Field-of-View Angle Constraints |
|---|---|
| Original language | Chinese (Traditional) |
| Pages (from-to) | 392-400 |
| Number of pages | 9 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 39 |
| Issue number | 4 |
| DOIs | |
| State | Published - 28 Apr 2018 |
Fingerprint
Dive into the research topics of 'Integrated Guidance and Control for A Strap-down Missile Considering Body Field-of-View Angle Constraints'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver