Reprogrammable Radar Tuning for Flight Phases, Environments, and Missions

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Solution Overview

Problem

Current millimeter wave frequency-modulated continuous-wave radars for aircraft have conflicting operational requirements for different functions, necessitating multiple radar systems that increase size, weight, complexity, and cost.

Innovation Solution

A reprogrammable radar system with a controller that adjusts radar parameters based on flight phase, environmental conditions, and mission requirements, allowing a single system to perform multiple functions optimally.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple different radar systems are installed to perform all desired functions, then operational optimality for all functions is achieved, but size, weight, complexity, and cost increase

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

Solution Approach 1:

The radar system is designed as a universal platform that can perform multiple functions (assisted landing, cable warning, sense and avoid) through software reconfiguration rather than requiring separate dedicated radar systems for each function. The controller can be reprogrammed to change radar parameters and operational modes, allowing one physical system to fulfill multiple operational roles.

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

Solution Approach 2:

The radar system incorporates dynamic reconfigurability where operational parameters such as frequency modulation characteristics, pulse repetition rates, and beam patterns can be changed in real-time based on the current mission requirements. This dynamic adaptation allows the same hardware to optimize its performance for different functions without physical reconfiguration.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If multiple different radar systems are installed to perform all desired functions, then operational optimality for all functions is achieved, but size and weight increase

Engineering Contradiction:
Improvefunctional versatilityVSAvoidaircraft weight
Core Design Contradiction:
Adaptability or versatilityVSWeight of moving object

Solution Approach 1:

Multiple radar functions that would traditionally require separate physical systems are merged into a single integrated radar platform. The transmit antenna, receive antenna, and controller are shared resources that serve multiple missions through software-defined operations, thereby eliminating the need for duplicate hardware and reducing overall system weight.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

A universal radar system design allows one physical apparatus to perform assisted landing, cable warning, and sense and avoid functions by reconfiguring operational parameters, thereby replacing multiple specialized radars and reducing the total weight burden on the aircraft.

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

3Device complexity

If a single fixed configuration radar system is used, then device complexity is reduced, but operational optimality for non-configured functions deteriorates

Engineering Contradiction:
Improvesystem complexityVSAvoidfunctional adaptability
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The radar system enables functional adaptation through changes in operational parameters such as frequency sweep characteristics, pulse duration, power levels, and scanning patterns. These parameter modifications allow the same hardware configuration to optimize performance for different missions without requiring physical reconfiguration or adding system complexity.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The system transitions from a static fixed configuration to a dynamic reconfigurable architecture where the controller can adjust operational parameters in real-time based on mission requirements, maintaining simplicity in hardware while achieving versatility through software-controlled parameter variation.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS12366655B2Reprogrammable radar system and method
Publication Date: 2025.07.22 ROCKWELL COLLINS INC
  • US12366655B2 patent drawing
  • US12366655B2 patent drawing
  • US12366655B2 patent drawing

AI summary

A system including a radar system. The radar system may include a transmit antenna, a receive antenna, and a controller. The controller may be configured to: determine or obtain information indicative of at least one of a phase of flight or an environmental condition; determine or obtain information indicative of a mission associated with the determined phase of flight and/or environmental condition; and based at least on the determined mission and the determined phase of flight and/or the environmental condition, tune radar parameters of the radar system to values to fulfill the determined mission associated with the determined phase of flight and/or environmental condition. The radar system may be reprogrammable by tuning the radar parameters to operate over any of a collection of phases of flight, any of a collection of environmental conditions, and any of a collection of missions.