Abstract
A 3-D integrated guidance and control (IGC) law for divert and attitude control system (DACS)-based strapdown interceptor subjected to strong couplings and complex constraints is proposed in this article. The 3-D kinematic and dynamic equations reflecting the couplings of the interceptor are constructed by combining the characteristics of DACS and strapdown seeker. An improved IGC model is established by employing the proposed adaptive fixed-time prescribed performance function (AFTPPF). This model takes into account the boundary, terminal, and convergence time constraints of strapdown interceptor, along with the mismatched unknown uncertainties. An IGC law is developed within the high-order multidimensional sliding mode control framework, integrating the AFTPPF to handle the complex constrains without computational singularities and the extended disturbance observer for uncertainty estimations. Finally, the stability and performance of the proposed control method are proved.
| Original language | English |
|---|---|
| Pages (from-to) | 9331-9344 |
| Number of pages | 14 |
| Journal | IEEE Transactions on Aerospace and Electronic Systems |
| Volume | 62 |
| DOIs | |
| State | Published - 2026 |
Keywords
- 3-D integrated guidance and control (IGC)
- divert and attitude control system (DACS)
- prescribed performance function (PPF)
- strapdown interceptor
Fingerprint
Dive into the research topics of '3-D Integrated Guidance and Control for Strapdown Interceptor under Divert and Attitude Control System'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver