Abstract
The presence of unmeasured parameters and unknown disturbances presents substantial challenges in the controller design of the Mars landing mission. In this article, the problem of adaptive prescribed-time tracking control for the powered descent phase of Mars landing with time-varying output constraints, unmeasured input deadzone nonlinearity, unknown vehicle mass, and disturbances is addressed. First, a prescribed-time output-constrained function is defined, and a class of time-varying barrier Lyapunov functions (BLFs) is developed, including estimation error information for disturbances and system parameters. Then, based on these functions and Nussbaum-type functions, an adaptive prescribed-time tracking control scheme is proposed for the powered descent phase of Mars landing in the presence of time-varying output constraints, unmeasured input deadzone nonlinearity, and unknown vehicle mass such that the tracking error converges to zero in a prescribed time and the control signals are bounded. Finally, several numerical simulations validate the effectiveness of the proposed method.
| Original language | English |
|---|---|
| Article number | 3005412 |
| Journal | IEEE Transactions on Instrumentation and Measurement |
| Volume | 74 |
| DOIs | |
| State | Published - 2025 |
| Externally published | Yes |
Keywords
- Adaptive prescribed-time tracking control
- barrier Lyapunov functions (BLFs)
- output-constrained system
- unknown vehicle mass
- unmeasured input deadzone nonlinearity
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