Distributed Engine Control Loop Encryption for Speed and Security
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Solution Overview
Problem
Aerospace control systems face challenges with existing encryption methods that increase system weight and certification costs due to uniform encryption across inner and outer control loops, and require more robust encryption in the outer loop for security, which can slow down communication.
Innovation Solution
Implementing a distributed engine control network with separate encryption levels in the inner and outer control loops, where the inner loop uses unencrypted or weaker encryption for faster communication and the outer loop employs encrypted data for security, optimizing encryption functionality and reducing system weight and certification costs.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If uniform encryption is applied across inner and outer control loops, then security is improved, but system weight and certification costs increase
Solution Approach 1:
The patent segments the control system into inner and outer control loops with different encryption requirements. The outer loop (non-safety-critical) uses encryption while the inner loop (safety-critical) uses unencrypted communication, dividing the system to apply appropriate security measures only where needed, thereby reducing overall system weight and certification burden while maintaining necessary security.
Solution Approach 2:
The patent applies different encryption qualities to different parts of the control system. The outer control loop receives encrypted data from sensors, while the inner control loop uses unencrypted data for real-time control. This local differentiation of security quality ensures security where needed without unnecessarily increasing system weight and certification costs in time-critical paths.
2Reliability
If uniform encryption is applied across inner and outer control loops, then security is improved, but certification costs increase
Solution Approach 1:
The patent segments the control system into inner and outer control loops with different encryption requirements. The outer loop (non-safety-critical) uses encryption while the inner loop (safety-critical) uses unencrypted communication, dividing the system to apply appropriate security measures only where needed, thereby reducing overall system weight and certification burden while maintaining necessary security.
Solution Approach 2:
The patent applies different encryption qualities to different parts of the control system. The outer control loop receives encrypted data from sensors, while the inner control loop uses unencrypted data for real-time control. This local differentiation of security quality ensures security where needed without unnecessarily increasing system weight and certification costs in time-critical paths.
3Reliability
If robust encryption is applied in the outer loop, then security is improved, but communication speed decreases
Solution Approach 1:
The patent segments the control system into inner and outer control loops with different encryption requirements. The outer loop (non-safety-critical) uses encryption while the inner loop (safety-critical) uses unencrypted communication, dividing the system to apply appropriate security measures only where needed, thereby reducing overall system weight and certification burden while maintaining necessary security.
Solution Approach 2:
The patent applies different encryption qualities to different parts of the control system. The outer control loop receives encrypted data from sensors, while the inner control loop uses unencrypted data for real-time control. This local differentiation of security quality ensures security where needed without unnecessarily increasing system weight and certification costs in time-critical paths.
Data Source
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AI summary
Methods and systems are provided for controlling a component of an aircraft engine (112) by communicating data over an inner control loop portion (118) of a distributed engine control network (102) for an aircraft (202); and controlling an operation of the aircraft engine (112) by communicating encrypted data over an outer control loop portion (120) of the distributed engine control network (102), wherein the data communicated over the inner control loop portion (118) is unencrypted or encrypted with weaker encryption than the data communicated over the outer control loop portion (120).