Balloon Payload Despin Control with Flexible Coupling Feedback

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Solution Overview

Problem

High-altitude balloons used in communication networks face challenges due to tilting, which impairs communication performance and requires maintaining solar panels and communication systems in optimal orientations, while flexible couplings introduce torsional flexibility that complicates orientation control.

Innovation Solution

A system comprising a flexible coupling, sensors to measure rotational displacement, and a despin mechanism with a motor and controller to maintain preferred orientations of payloads, using torque control and temperature measurements to counteract tilting and torsional effects.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a flexible coupling is used to accommodate balloon envelope tilting, then the payload can tolerate tilt effects, but orientation control precision deteriorates due to torsional flexibility

Engineering Contradiction:
Improvetilt accommodationVSAvoidorientation control precision
Core Design Contradiction:
Adaptability or versatilityVSManufacturing precision

Solution Approach 1:

The system employs sensors (encoders, strain gauges, potentiometers) to continuously measure the rotational displacement and torque of the flexible coupling, feeding this information back to the controller. The controller dynamically adjusts the despin mechanism to compensate for the coupling's flexibility, thereby maintaining precise payload orientation despite the torsional compliance of the coupling.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent replaces direct mechanical rigid coupling with a flexible coupling that introduces controlled torsional compliance. This substitution allows the system to accommodate balloon tilting while the control system uses sensors and active feedback to maintain orientation precision, effectively replacing pure mechanical precision with a combination of flexible mechanics and active control.

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

2Reliability

If a despin mechanism is used to maintain payload orientation, then communication and solar panel performance improve, but device complexity increases

Engineering Contradiction:
Improvecommunication performanceVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The despin mechanism serves multiple functions: it maintains payload orientation for communication systems, ensures optimal solar panel alignment for power generation, and compensates for the flexible coupling's torsional movements. By consolidating these functions into a single controlled mechanism, the system achieves improved reliability across multiple subsystems without proportionally increasing overall complexity.

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

Solution Approach 2:

The flexible coupling acts as an intermediary element between the rigid payload and the tilting balloon envelope. It isolates the payload from direct mechanical tilting forces while allowing the despin mechanism to work with reduced mechanical stress, thereby improving communication and power system reliability while managing the complexity of the control system.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Manufacturing precision

If temperature compensation is implemented for flexible coupling stiffness, then orientation accuracy improves, but measurement and control complexity increases

Engineering Contradiction:
Improveorientation accuracyVSAvoidtemperature measurement complexity
Core Design Contradiction:
Manufacturing precisionVSDifficulty of detecting and measuring

Solution Approach 1:

Temperature sensors (thermistors, thermocouples) continuously monitor the temperature of the flexible coupling and feed this data back to the controller. The controller uses this temperature information to dynamically adjust the despin mechanism's operation, compensating for temperature-induced stiffness changes in the coupling and thereby maintaining high orientation accuracy.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system explicitly accounts for and compensates for changes in the flexible coupling's physical parameters (stiffness) as a function of temperature. By measuring temperature and adjusting control parameters accordingly, the system maintains orientation accuracy despite environmental temperature variations that would otherwise alter the coupling's mechanical properties.

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

The system effectively reduces payload tilt, maintains optimal orientations for communication and solar panel alignment, and manages torsional flexibility to enhance communication performance and power collection.

Implementation Method 1

a flexible coupling configured to reduce effects of a balloon envelope tilting on a payload

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

the sensor is a magnetic encoder

Methodology Applied
Scientific EffectMagnetic field detection: Magnetic Field

Implementation Method 3

the sensor is an optical encoder

Methodology Applied
Scientific EffectOptical detection: Light

Implementation Method 4

a despin mechanism including a motor configured to rotate the payload

Methodology Applied
Scientific EffectElectromagnetic conversion: Electromagnetic Induction

Implementation Method 5

a thermometer configured to measure temperature of the flexible coupling

Methodology Applied
Scientific EffectThermal detection: Temperature Gradient

Data Source

PatentUS11981450B2Torque control for balloon coupling
Publication Date: 2024.05.14 AEROSTAR INT LLC
  • US11981450B2 patent drawing
  • US11981450B2 patent drawing
  • US11981450B2 patent drawing

AI summary

Aspects of the disclosure provide for controlling orientation of a payload of a balloon through a despin mechanism. In one instance, a system may include a flexible coupling configured to reduce effects of a balloon envelope tilting on a payload, a sensor configured to measure rotational displacement of the flexible coupling, a despin mechanism including a motor configured to rotate the payload, and a controller. The controller may be configured to use receive the measured rotational displacement and to use the despin mechanism to rotate the payload towards a preferred orientation based on the measured rotational displacement.