CubeSat RF Frontend Architecture for Versatile Radar Operations

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Solution Overview

Problem

Current microsatellite-compatible RF systems are low-performance and often custom-designed for specific applications, occupying valuable space, mass, and power resources without providing adequate functionality for diverse missions like broadband communications and RF signal collection.

Innovation Solution

A high-performance, flexible RF system architecture that includes a digital-to-analog converter, transmitter, receiver, analog-to-digital converter, and non-volatile storage interfaces, with a programmable logic device for efficient data processing and storage, enabling radar operations between 100 MHz and 9 GHz with reduced power and cost.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If current microsatellite-compatible RF systems are used, then space, mass, and power resources are occupied, but performance is low and functionality is limited to specific applications

Engineering Contradiction:
Improvemission versatilityVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent implements a universal RF system architecture that can perform multiple functions including radar operations, broadband communications, and RF signal collection through reconfigurable hardware components. The system uses programmable logic devices and configurable signal processing paths to adapt to different mission requirements, eliminating the need for separate specialized systems for each application.

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

2Adaptability or versatility

If current RF systems are used, then space and mass are occupied, but the hardware is too generalized and provides unwanted functionality

Engineering Contradiction:
Improvefunctional flexibilityVSAvoidpower consumption
Core Design Contradiction:
Adaptability or versatilityVSUse of energy by moving object

Solution Approach 1:

The system employs dynamic reconfiguration capabilities where hardware components can be programmed and adjusted in real-time to match current mission needs. The programmable logic device and configurable signal processing chain allow the system to activate only the necessary functional blocks for each operation, reducing power consumption by keeping unused components in low-power states.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent utilizes parameter changes in hardware configuration to adapt system behavior. By modifying register settings, clock distributions, and signal routing parameters, the same physical hardware can transition between different operational modes (radar transmit, radar receive, communications), enabling functional flexibility without adding physical components.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If current RF systems are used, then space, mass, and power budget are consumed, but no benefit is provided for unwanted functionality

Engineering Contradiction:
Improvedata storage bandwidthVSAvoidspace and mass
Core Design Contradiction:
ProductivityVSQuantity of substance

Solution Approach 1:

The patent segments the data storage function into multiple parallel non-volatile storage interfaces. Instead of using a single high-bandwidth storage interface that would require significant space and power, the system divides the data stream across multiple storage channels, achieving high overall bandwidth while using smaller, more space-efficient storage components.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system transitions from a single-dimensional storage approach to a multi-dimensional storage architecture by implementing parallel storage interfaces and distributed data buffering. This dimensional change in the storage architecture enables high data bandwidth to be achieved through spatial distribution rather than requiring a single high-capacity storage device that would consume excessive space and mass.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Data Source

PatentUS11385327B2CubeSat radar systems
Publication Date: 2022.07.12 SRI INTERNATIONAL
  • US11385327B2 patent drawing
  • US11385327B2 patent drawing
  • US11385327B2 patent drawing

AI summary

Implementation of radio frequency applications in satellite environments can be constrained by size, mass, cost, and power limitations. These applications can include radar, communications, radio astronomy, or other scientific or industrial applications. A variety of systems are provided to facilitate recording of baseband radio frequency signals at high bandwidth and low power using low-cost components. These systems include field-programmable gate arrays or other programmable logic devices integrating between high-frequency ADCs and two or more multiplexed non-volatile storage mediums. Also provided are systems for providing calibration and self-test functionality in a low-cost, flexible, low-power radio frequency frontend. These systems include high-frequency switches configured to allow a calibration and/or self-test pulse to be acquired for each radar pulse generated by the system.