Abstract
This paper considers a class of thrust vectoring systems, which are nonlinear, overactuated, and time-invariant. We assume that the system is composed of two subsystems and there exist singular points around which the linearized system is uncontrollable. Furthermore, we assume that the system is stabilizable through a two-level control allocation. In this particular setting, we cannot do much with the linearized system, and a direct nonlinear control approach must be used to analyze the system stability. Under adequate assumptions and a suitable nonlinear continuous control-allocation law, we can prove uniform asymptotic convergence of the points of equilibrium using Lyapunov input-to-state stability and the small gain theorem. This control allocation, however, requires the design of an allocated mapping and introduces two exogenous inputs. In particular, the closed-loop system is cascaded, and the output of one subsystem is the disturbance of the other, and vice versa. In general, it is difficult to find a closed-form solution for the allocated mapping; it needs to satisfy restrictive conditions, among which Lipschitz continuity to ensure that the disturbances eventually vanish. Additionally, this mapping is in general nontrivial and non-unique. In this paper, we propose a new kernel-based predictive control allocation to substitute the need for designing an analytic mapping, and assess if it can produce a meaningful mapping “on-the-fly” by solving online an optimization problem. The simulations include two examples, which are the manipulation of an object through an unmanned aerial vehicle in three dimensions, and the control of a surface vessel actuated by two azimuthal thrusters.
| Original language | English |
|---|---|
| Article number | 112270 |
| Journal | Automatica |
| Volume | 177 |
| DOIs | |
| State | Published - Jul 2025 |
Keywords
- Application of nonlinear analysis and design
- Control allocation
- Model predictive control
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