Balloon Reflector Feed Steering With Tethered Drones

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Solution Overview

Problem

Existing balloon reflector antennas are unable to quickly steer their beams to track fast-moving terrestrial or orbiting objects due to limitations in their feed systems, which are inadequate for high-altitude operations with diameters larger than 5 meters.

Innovation Solution

A large balloon reflector antenna system with a near-spherical reflective surface and a feed system that includes drones equipped with transmission/detection systems, capable of steering the beam using retractable tethers and optics modules for precise positioning and correction, allowing for rapid target tracking across a wide field of view.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If conventional feed systems are used in large balloon reflector antennas, then the antenna can be manufactured with simpler technology, but the beam steering speed is too slow to track fast-moving objects

Engineering Contradiction:
Improvebeam steering speedVSAvoidfeed system complexity
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The feed system is divided into multiple independent drone units, each capable of autonomous positioning and beam formation. This segmentation allows parallel operation of multiple feed elements, enabling rapid beam steering without moving the entire antenna structure, thus achieving high-speed tracking while maintaining manageable system complexity through modular architecture

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The feed system transitions from a static conventional structure to a dynamic multi-drone configuration where individual feed elements can independently reposition themselves in three-dimensional space. This dynamic reconfigurability enables real-time beam steering by adjusting the relative positions and phases of distributed feed elements, achieving fast tracking speeds adaptable to different operational requirements

Inventive Principle:
Principle #15Dynamics

2Area of moving object

If the balloon reflector diameter is increased to improve gain and resolution, then the antenna performance improves, but the feed system becomes inadequate for high-altitude operations

Engineering Contradiction:
Improvereflector aperture areaVSAvoidfeed system reliability at high altitude
Core Design Contradiction:
Area of moving objectVSReliability

Solution Approach 1:

The drone-based feed system provides multi-functionality by combining positioning, signal transmission, and beam forming capabilities in single units. These universal feed elements can operate effectively across large reflector apertures while adapting to high-altitude environmental conditions, ensuring reliable performance regardless of balloon size or operational altitude

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The feed drones are equipped with autonomous navigation and positioning systems that enable self-service operation at high altitudes. Each drone independently manages its position, orientation, and signal transmission without requiring complex ground-based control infrastructure, ensuring feed system reliability in the challenging high-altitude environment through self-contained operational capabilities

Inventive Principle:
Principle #25Self-service

3Ease of operation

If a pivoting line feed or phased array is used, then beam steering is possible, but the entire structure must be repositioned which increases size, weight, and cost

Engineering Contradiction:
Improvebeam steering capabilityVSAvoidantenna system weight
Core Design Contradiction:
Ease of operationVSWeight of moving object

Solution Approach 1:

The mechanical beam steering mechanism is replaced with an electromagnetic field-based solution using distributed drone feed elements. Instead of physically repositioning heavy antenna structures or pivoting large feed assemblies, the system electronically steers beams by adjusting the phase and amplitude of signals from individually controllable drone-based feed elements, eliminating the need for mechanical repositioning infrastructure and significantly reducing system weight

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

Beam steering is achieved by changing electromagnetic parameters (phase, amplitude, frequency) of the feed signals rather than changing the physical position of the entire antenna structure. The drone-based feed system dynamically adjusts these parameters to steer beams rapidly, providing ease of operation through electronic control while avoiding the weight penalties associated with mechanical repositioning systems

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables effective target tracking of fast-moving objects from stratospheric altitudes, providing a high-gain antenna system suitable for radio to infrared wavelengths with extended operational duration and remote sensing capabilities.

Implementation Method 1

a near-spherical reflective surface formed on an interior surface of the balloon opposite the transparent surface

Methodology Applied
Scientific EffectReflection: Reflection

Implementation Method 2

Existing balloon reflector antennas (e.g., as described below with reference to FIG. 1) include a transparent surface opposite a reflective surface. Electromagnetic waves pass through the transparent surface and are reflected off the reflective surface of the balloon reflector.

Methodology Applied
Scientific EffectTransmission:

Data Source

PatentUS20240363991A1Large balloon reflector for remote sensing
Publication Date: 2024.10.31 THE ARIZONA BOARD OF REGENTS ON BEHALF OF THE UNIV OF ARIZONA
  • US20240363991A1 patent drawing
  • US20240363991A1 patent drawing
  • US20240363991A1 patent drawing

AI summary

A large balloon reflector, capable of launching and support itself at high altitudes, with a feed system capable of steering the beam quickly enough to perform target tracking of fast-moving terrestrial, stratospheric, or orbiting objects. The large balloon reflector antenna forms a suborbital antenna system that is suitable for operation from radio to infrared wavelengths and can be used, for example, for remote sensing of objects on the ground, in the atmosphere, or in space.