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Design and Autonomous Stabilization of a Ballistically Launched Multirotor (1911.10269v2)

Published 22 Nov 2019 in eess.SY, cs.RO, and cs.SY

Abstract: Aircraft that can launch ballistically and convert to autonomous, free flying drones have applications in many areas such as emergency response, defense, and space exploration, where they can gather critical situational data using onboard sensors. This paper presents a ballistically launched, autonomously stabilizing multirotor prototype (SQUID, Streamlined Quick Unfolding Investigation Drone) with an onboard sensor suite, autonomy pipeline, and passive aerodynamic stability. We demonstrate autonomous transition from passive to vision based, active stabilization, confirming the ability of the multirotor to autonomously stabilize after a ballistic launch in a GPS denied environment.

Citations (14)

Summary

  • The paper demonstrates SQUID’s innovative integration of ballistic launch with active stabilization for seamless autonomous flight.
  • The paper outlines a robust design featuring foldable arms and aerodynamic fins that provide passive stability during high-g ballistic phases.
  • The paper validates the approach through controlled tests and wind tunnel experiments, highlighting its potential for rapid deployment in constrained environments.

Summary of "Design and Autonomous Stabilization of a Ballistically-Launched Multirotor"

This paper discusses a novel approach to multirotor deployment through the design and testing of the Streamlined Quick Unfolding Investigation Drone (SQUID), a prototype capable of ballistic launches and autonomous stabilization. The work presents advancements in aerial system deployment in scenarios where conventional launches are impractical, such as in emergency response, defense, and space exploration.

Mechanical and Aerodynamic Design

The paper outlines the mechanical construction of SQUID, emphasizing the requirements for launching from a constrained space, such as a tube, and transitioning to stable autonomous flight. Key features include a robust carbon fiber frame, foldable arms, and fins for aerodynamic stability, allowing it to launch ballistically and unfold in mid-air.

The folding fins are a critical design element that impart passive aerodynamic stability during the multirotor's ballistic phase, ensuring that the aerodynamic center trails behind the center of mass. This configuration enables the multirotor to naturally align with its direction of travel, enhancing its stability upon launch. The airframe supports the g-forces of launch effectively, sustaining onboard payload and structural integrity.

Transition from Ballistic Launch to Autonomous Control

Following launch, the onboard system transitions from passive to active stabilization. Initially, the crafted aerodynamic design controls orientation without active feedback. As the multirotor nears apogee, the motors activate, engaging the stabilization process. The paper describes the use of a robust visual-inertial odometry pipeline that facilitates vision-based active stabilization in GPS-denied environments.

The transition timing is crucial. The motors must engage within the ballistic phase, prior to reaching apogee, so the multirotor stabilizes before aerodynamic forces are insufficient at slower speeds. The visual-inertial odometry system utilizes tight integration of camera and inertial data, enabling the multirotor to stabilize even in low-texture environments.

Experimental Validation

The SQUID prototype's viability is validated through a series of controlled indoor test launches. A combination of passive aerodynamic stability and advanced active stabilization allows it to achieve a seamless transition from a ballistic launch to autonomous flight. Subscale wind tunnel tests and full-scale experiments confirmed the system's predictable behavior in various launch conditions.

Implications and Future Developments

This research has significant implications for enhancing deployment capabilities of aerial systems in dynamic and constrained environments. The successful integration of ballistic launch and autonomous stabilization extends the operational scope of multirotors, providing opportunities to deploy aerial platforms swiftly and safely in scenarios where conventional multirotor deployment would be infeasible.

Future developments may include enhancements to the passive stabilization mechanism to accommodate a wider range of operational conditions, such as stronger crosswinds during launches from moving vehicles. Additionally, further refinement of the onboard software to allow quicker initialization and stabilization upon launch would enhance system responsiveness and reliability.

In conclusion, the SQUID prototype demonstrates an innovative solution to extend the deployment flexibility and operational efficiency of multirotor systems. The findings pave the way for future applications in diverse fields requiring rapid aerial deployment capabilities. The proof-of-concept successfully shows a feasible path toward practical implementation in complex operational environments.

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