Abstract
Purpose: The purpose of this paper is to present a high accuracy path following method for low-cost fixed-wing UAVs. Design/methodology/approach: The original vector field (VF) algorithm is condensed. A spatial integration mechanism is added to the existing VF and nonlinear guidance law, aiming to decrease steady-state cross-track-error and cope with long-term disturbance. Findings: Numerical simulations show the proposed method could diminish steady-state cross-track-error effectively. Test flights show the proposed method is applicable on low-cost fixed-wing UAVs. Practical implications: The path following accuracy shown in simulations and test flights indicates the proposed method could be deployed in scenarios including inflight rendezvous, formation, trafficway take-off and landing. Originality/value: This paper provides an improved high-accuracy path following method for low-cost fixed-wing UAVs.
| Original language | English |
|---|---|
| Pages (from-to) | 20-28 |
| Number of pages | 9 |
| Journal | Aircraft Engineering and Aerospace Technology |
| Volume | 94 |
| Issue number | 11 |
| DOIs | |
| State | Published - 2022 |
| Externally published | Yes |
Keywords
- Flight control
- Flight test
- Nonlinear guidance law
- Path following
- UAV
- Vector field
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