pith. sign in

arxiv: 2607.02478 · v1 · pith:4GCIVNZDnew · submitted 2026-07-02 · 📡 eess.SY · cs.SY

Docking of Autonomous Vehicles with a Stationary Docking Station in 3D Space

Pith reviewed 2026-07-03 07:19 UTC · model grok-4.3

classification 📡 eess.SY cs.SY
keywords autonomous dockingsliding mode controlline-of-sight kinematicsfinite-time convergence3D vehicle guidancerange-based control
0
0 comments X

The pith

A finite-time sliding mode strategy using range and line-of-sight kinematics achieves safe autonomous docking in 3D space.

A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.

This paper develops a control method for autonomous vehicles to dock with a fixed station in three-dimensional environments. The method ensures the vehicle reaches a specific orientation relative to the station while slowing to nearly zero speed to avoid collision. It draws on guidance principles to design a sliding mode controller that converges in finite time. The design uses only measurements of distance and line-of-sight angles between the vehicle and station. This matters because docking is safety-critical in applications like aerial, marine, and space vehicles where precise alignment is needed.

Core claim

The paper presents a finite-time sliding mode-based strategy that uses range and line-of-sight kinematics relations to steer the vehicle to the desired orientation for docking and reduce its speed to near-zero.

What carries the argument

finite-time sliding mode control law derived from range and line-of-sight kinematics relations

If this is right

  • The vehicle achieves the required orientation and terminal speed from a range of initial positions and attitudes.
  • The controller relies solely on range and line-of-sight information rather than full dynamic models.
  • MATLAB simulations confirm successful docking across varied initial locations and orientations of both vehicle and station.

Where Pith is reading between the lines

These are editorial extensions of the paper, not claims the author makes directly.

  • Practical deployment would need additional compensation for disturbances and actuator constraints omitted from the kinematic model.
  • The same kinematic sliding-mode structure could be adapted for docking with a moving station by updating the reference kinematics.
  • The finite-time property may permit explicit bounds on docking duration once the gain parameters are fixed.

Load-bearing premise

The range and line-of-sight kinematics relations describing the motion of the vehicle with respect to the stationary docking station are sufficient to design a control law that achieves safe docking.

What would settle it

A simulation in which the vehicle under the proposed control law fails to reach the desired orientation or near-zero speed for at least one set of initial conditions satisfying the kinematic model.

Figures

Figures reproduced from arXiv: 2607.02478 by Hemendra Arya, Ram Milan Kumar Verma, Shashi Ranjan Kumar.

Figure 2
Figure 2. Figure 2: Approach angle of the vehicle to the docking station. Problem 1: Consider the engagement scenario as repre￾sented in [PITH_FULL_IMAGE:figures/full_fig_p002_2.png] view at source ↗
Figure 1
Figure 1. Figure 1: shows the representation of the geometric engagement [PITH_FULL_IMAGE:figures/full_fig_p002_1.png] view at source ↗
Figure 3
Figure 3. Figure 3: Demonstration of docking for various initial locations of the vehicle while fixed docking station. 0 15 5 10 10 Z m ( ) 10 15 Y (m) 5 X (m) 20 0 0 -5 -10 D1 D2 D3 (a) Path of the vehicle. 0 10 20 30 40 VU ( m / s ) 0 2 4 D1 D2 D3 0 10 20 30 40 R ( m ) 0 10 20 Time (s) 0 10 20 30 40 _R ( m / s ) -2 -1 0 (b) Speed, range and closing rate. a 0 10 20 30 40 U x ( m / s 2 ) 0 1 2 3 D1 D2 D3 a 0 10 20 30 40 U y (… view at source ↗
Figure 4
Figure 4. Figure 4: Demonstration of docking for various locations of the docking station while fixed vehicle initial location. 10 X (m) 0 5 10 2 Z 4 ( m )6 5 Y (m) 0 8 10 0 App1 App2 App3 (a) Path of the vehicle. 0 10 20 30 40 VU ( m / s ) 0 1 2 App1 App2 App3 0 10 20 30 40 R ( m ) 0 10 20 Time (s) 0 10 20 30 40 _R ( m / s ) -1 -0.5 0 (b) Speed, range and closing rate. a 0 10 20 30 40 U x ( m / s 2 ) 0 0.5 1 App1 App2 App3 a… view at source ↗
Figure 5
Figure 5. Figure 5: Demonstration of docking for various approach angles with the same docking station location and initial vehicle location. [3] D.-j. Li, Y.-h. Chen, J.-g. Shi, and C.-j. Yang, “Autonomous underwater vehicle docking system for cabled ocean observatory network,” Ocean Engineering, vol. 109, pp. 127–134, 2015. [4] Y. Li, Y. Jiang, J. Cao, B. Wang, and Y. Li, “AUV docking experiments based on vision positioning… view at source ↗
read the original abstract

In this letter, we present a strategy for autonomous docking of autonomous vehicles in three-dimensional space. Docking is a safety-critical task and requires expert piloting skills. Vehicles with autonomous docking capabilities are highly desirable in various applications, such as marine vehicle docking, aerial vehicle docking, spacecraft docking, and landing. To dock autonomously with the docking station, the vehicle must align itself to a specific desired orientation relative to the docking station and also reduce speed as it approaches. The vehicle achieves near-zero speed to dock successfully and safely without colliding with the docking station. Inspired by the philosophies from the guidance literature, we present a finite-time sliding mode-based strategy to achieve the same. The range and line-of-sight kinematics relations describing the motion of the vehicle with respect to the stationary docking station are used to steer the vehicle to achieve the desired orientation for docking. This docking strategy is validated in MATLAB\textsuperscript{\textregistered} simulations for various initial locations and orientations of both the vehicle and the docking station.

Editorial analysis

A structured set of objections, weighed in public.

Desk editor's note, referee report, simulated authors' rebuttal, and a circularity audit. Tearing a paper down is the easy half of reading it; the pith above is the substance, this is the friction.

Referee Report

2 major / 0 minor

Summary. The paper proposes a finite-time sliding-mode control strategy for autonomous 3D docking of vehicles with a stationary station. The approach uses range and line-of-sight (LOS) kinematics to generate commands that align the vehicle to a desired orientation while driving relative speed to near zero; the law is derived from standard guidance relations and validated only via MATLAB simulations across varied initial conditions.

Significance. If the kinematic convergence result transfers to a closed-loop dynamic system, the method would supply a simple, parameter-light guidance law for safety-critical docking tasks in marine, aerial, and spacecraft applications. The manuscript supplies no machine-checked proofs, reproducible code, or falsifiable dynamic predictions, so its contribution rests entirely on the simulation outcomes.

major comments (2)
  1. [Abstract and kinematics-usage paragraph] Abstract and the paragraph on kinematics usage: the finite-time sliding-mode commands are derived directly from the range and LOS rate equations, treating these kinematic relations as the plant. No 6-DOF rigid-body equations, inertia matrix, thrust mapping, saturation limits, or disturbance model appear, so the proven convergence on the kinematic manifold does not automatically transfer to the physical vehicle.
  2. [Simulation validation] Simulation validation section: all reported trials assume perfect velocity tracking with no sensor noise, external disturbances, or actuator dynamics. This leaves the central safety claim (near-zero speed docking without collision) supported only under idealized conditions that match the omitted dynamics.

Simulated Author's Rebuttal

2 responses · 0 unresolved

We thank the referee for the detailed and constructive feedback. Our response addresses each major comment in turn, clarifying the intended kinematic scope of the work while acknowledging its limitations.

read point-by-point responses
  1. Referee: [Abstract and kinematics-usage paragraph] Abstract and the paragraph on kinematics usage: the finite-time sliding-mode commands are derived directly from the range and LOS rate equations, treating these kinematic relations as the plant. No 6-DOF rigid-body equations, inertia matrix, thrust mapping, saturation limits, or disturbance model appear, so the proven convergence on the kinematic manifold does not automatically transfer to the physical vehicle.

    Authors: The manuscript intentionally develops and analyzes the guidance law at the kinematic level using range and line-of-sight relations, as is common in the guidance literature for deriving commands that can later be tracked by an inner-loop dynamic controller. Convergence is established for the kinematic system, and the approach assumes perfect command tracking by lower-level controllers (a standard cascaded structure). We agree that this does not automatically guarantee performance on a full 6-DOF vehicle with inertia, saturation, or disturbances. In revision we will explicitly state the kinematic scope in the abstract and introduction and add a brief note on the required inner-loop assumption. revision: partial

  2. Referee: [Simulation validation] Simulation validation section: all reported trials assume perfect velocity tracking with no sensor noise, external disturbances, or actuator dynamics. This leaves the central safety claim (near-zero speed docking without collision) supported only under idealized conditions that match the omitted dynamics.

    Authors: The simulations validate the kinematic law under ideal velocity tracking, which is the appropriate test for a guidance strategy before dynamic integration. We acknowledge that the safety claim (near-zero relative speed at docking) holds only under these idealized conditions and does not yet address noise or disturbances. In revision we will expand the discussion to highlight these assumptions and outline future dynamic validation steps, without altering the existing simulation results. revision: partial

Circularity Check

0 steps flagged

No circularity: derivation from standard range/LOS kinematics and sliding-mode guidance is independent

full rationale

The paper constructs its finite-time sliding-mode docking commands directly from the range and line-of-sight kinematic relations (abstract and kinematics-usage section), treating these as the plant model and citing external guidance literature for the underlying philosophy. No equation reduces by construction to a fitted parameter, self-referential quantity, or load-bearing self-citation chain; the central claim remains an independent mapping from the kinematic manifold to the control law. This is the most common honest finding for a kinematics-only guidance paper.

Axiom & Free-Parameter Ledger

0 free parameters · 2 axioms · 0 invented entities

The approach rests on standard sliding mode control assumptions and kinematic models; no new free parameters, axioms, or invented entities are introduced beyond those implicit in the cited guidance literature.

axioms (2)
  • domain assumption Finite-time convergence properties of sliding mode control hold when applied to the range and line-of-sight kinematic model.
    Invoked when stating the finite-time sliding mode strategy achieves the docking conditions.
  • domain assumption Range and line-of-sight kinematics accurately capture the relative motion needed for control design.
    Stated directly in the abstract as the basis for steering the vehicle.

pith-pipeline@v0.9.1-grok · 5712 in / 1426 out tokens · 32970 ms · 2026-07-03T07:19:41.186823+00:00 · methodology

discussion (0)

Sign in with ORCID, Apple, or X to comment. Anyone can read and Pith papers without signing in.

Reference graph

Works this paper leans on

17 extracted references

  1. [1]

    Tracking control of docking maneuvers for a fully actuated surface vessel using backstepping,

    L. M. Kinjo, T. M ´enard, S. Wirtensohn, O. Gehan, and J. Reuter, “Tracking control of docking maneuvers for a fully actuated surface vessel using backstepping,”IEEE Transactions on Control Systems Technology, vol. 32, no. 5, pp. 1920–1927, 2024

  2. [2]

    AUV homing and docking for remote operations,

    N. Palomeras, G. Vallicrosa, A. Mallios, J. Bosch, E. Vidal, N. Hurtos, M. Carreras, and P. Ridao, “AUV homing and docking for remote operations,”Ocean Engineering, vol. 154, pp. 106–120, 2018. 6 IEEE CONTROL SYSTEMS LETTERS, VOL. XX, NO. XX, XXXX 2017 0 5 Z (m) 0 10 X (m) 5 10 Y (m) 10 50 P1 P2 P3 (a) Path of the vehicle. 0 10 20 30 40 VU (m/s) 0 1 2 P1 ...

  3. [3]

    Autonomous underwater vehicle docking system for cabled ocean observatory network,

    D.-j. Li, Y .-h. Chen, J.-g. Shi, and C.-j. Yang, “Autonomous underwater vehicle docking system for cabled ocean observatory network,”Ocean Engineering, vol. 109, pp. 127–134, 2015

  4. [4]

    AUV docking experiments based on vision positioning using two cameras,

    Y . Li, Y . Jiang, J. Cao, B. Wang, and Y . Li, “AUV docking experiments based on vision positioning using two cameras,”Ocean Engineering, vol. 110, pp. 163–173, 2015

  5. [5]

    Robust aerial docking in carrier-centered frame: A relative state-based approach,

    X. Dong, Y . Cui, D. Li, B. Yang, J. Xiang, and Z. Tu, “Robust aerial docking in carrier-centered frame: A relative state-based approach,” IEEE Robotics and Automation Letters, vol. 11, no. 2, pp. 1802–1809, 2026

  6. [6]

    Real-time autonomous spacecraft proximity maneuvers and docking using an adap- tive artificial potential field approach,

    R. Zappulla, H. Park, J. Virgili-Llop, and M. Romano, “Real-time autonomous spacecraft proximity maneuvers and docking using an adap- tive artificial potential field approach,”IEEE Transactions on Control Systems Technology, vol. 27, no. 6, pp. 2598–2605, 2019

  7. [7]

    Robust model predictive control for spacecraft rendezvous under sector-bounded non- linearities,

    ´A. M. Bokor, F. Biert ¨umpfel, P. Seiler, and R. T ´oth, “Robust model predictive control for spacecraft rendezvous under sector-bounded non- linearities,”IEEE Control Systems Letters, vol. 9, pp. 2567–2572, 2025

  8. [8]

    Guaranteed safe spacecraft docking with control barrier functions,

    J. Breeden and D. Panagou, “Guaranteed safe spacecraft docking with control barrier functions,”IEEE Control Systems Letters, vol. 6, pp. 2000–2005, 2022

  9. [9]

    Three-dimensional mobile docking control method of an underactuated autonomous underwater vehicle,

    T. Xie, Y . Li, Y . Jiang, S. Pang, and X. Xu, “Three-dimensional mobile docking control method of an underactuated autonomous underwater vehicle,”Ocean Engineering, vol. 265, p. 112634, 2022

  10. [10]

    Autonomous underwater vehicle docking,

    J. G. Bellingham, “Autonomous underwater vehicle docking,” in Springer Handbook of Ocean Engineering, ser. Springer Handbooks, M. R. Dhanak and N. I. Xiros, Eds. Springer, 2016, pp. 387–406

  11. [11]

    A USV-based automated launch and recovery system for AUVs,

    E. I. Sarda and M. R. Dhanak, “A USV-based automated launch and recovery system for AUVs,”IEEE Journal of Oceanic Engineering, vol. 42, no. 1, pp. 37–55, 2017

  12. [12]

    Au- tonomous docking of hovering type AUV to seafloor charging station based on acoustic and visual sensing,

    Y . Sato, T. Maki, K. Masuda, T. Matsuda, and T. Sakamaki, “Au- tonomous docking of hovering type AUV to seafloor charging station based on acoustic and visual sensing,” in2017 IEEE Underwater Technology (UT), 2017, pp. 1–6

  13. [13]

    Three-dimensional impact angle guidance with coupled engagement dynamics,

    S. R. Kumar and D. Ghose, “Three-dimensional impact angle guidance with coupled engagement dynamics,”Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 231, no. 4, pp. 621–641, 2017

  14. [14]

    Spatial nonlinear guidance strategies for target interception at pre-specified orientation,

    R. V . Nanavati, S. R. Kumar, and A. Maity, “Spatial nonlinear guidance strategies for target interception at pre-specified orientation,”Aerospace Science and Technology, vol. 114, p. 106735, 2021

  15. [15]

    Three-dimensional impact angle constrained nonlinear guidance with predefined convergence time,

    K. Majumder and S. R. Kumar, “Three-dimensional impact angle constrained nonlinear guidance with predefined convergence time,” Nonlinear Dynamics, vol. 112, no. 12, pp. 9983–10 008, 2024

  16. [16]

    Quaternion-based non-singular nonlinear impact angle guidance for three-dimensional engagements,

    P. Surve, A. Maity, and S. R. Kumar, “Quaternion-based non-singular nonlinear impact angle guidance for three-dimensional engagements,” Aerospace Science and Technology, vol. 155, p. 109657, 2024

  17. [17]

    Autonomous docking of uncrewed surface vessel with stationary and moving ships,

    R. M. K. Verma, S. R. Kumar, and H. Arya, “Autonomous docking of uncrewed surface vessel with stationary and moving ships,”Journal of Guidance, Control, and Dynamics, vol. 49, no. 6, pp. 1860–1869, 2026