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DO-178B Risk Management For Airborne Systems

Table of Contents


DO-178B, formally known as “Software Considerations in Airborne Systems and Equipment Certification,” is a crucial standard within the aviation industry that has played a pivotal role in ensuring the safety and reliability of software used in airborne systems. Developed by the Radio Technical Commission for Aeronautics (RTCA) in collaboration with EUROCAE, this internationally recognized document sets forth stringent guidelines for the certification of software in civil aircraft, including both commercial and general aviation platforms. As the aviation sector continues to rely increasingly on complex software-driven systems, understanding DO-178B’s principles and practices is essential for aviation professionals, regulators, and engineers striving to maintain the highest safety standards in the skies. In this article, we delve into the key aspects of DO-178B, its evolution, and its enduring impact on the aviation industry.

What Is DO-178B?

Published in 1992 by the Radio Technical Commission for Aeronautics (RTCA) and developed jointly with EUROCAE, the European Organization for Civil Aviation Equipment, DO-178B is an international guideline that deals with the safety of mission-critical software used in airborne systems and equipment. Even though it is just a guideline and not a policy, DO-178B is seen as a standard for developing avionics software, and even the FAA uses it for guidance when determining if a piece of software will perform reliably in an airborne environment.

Despite being developed specifically to meet the unique needs of the aerospace industry, DO-178B has seen use in other industries as well, often in conjunction with DO-254, also known as Design Assurance Guidance for Airborne Electronic Hardware, which deals with the development of airborne electronic hardware. Just like DO-178B, DO-254 is published by RTCA, a United States volunteer organization whose mission is to develop technical guidance for use by government regulatory authorities and by industry.

Key Principles and Objectives of DO-178B

The key principles and objectives of DO-178B, formally known as “Software Considerations in Airborne Systems and Equipment Certification,” are fundamental to its role in ensuring the safety and reliability of software used in airborne systems. These principles and objectives guide the development and certification process, emphasizing safety and quality assurance. Here’s an explanation of the key principles and objectives of DO-178B:

  1. Safety-Critical Focus:
    • Principle: The primary principle of DO-178B is to address the safety-critical nature of software used in airborne systems. It recognizes that software failures in aviation can lead to catastrophic consequences.
    • Objective: The objective is to ensure that the software functions safely and reliably under all conditions, minimizing the risk of accidents or incidents caused by software-related failures.
  2. Requirements-Based Approach:
    • Principle: DO-178B promotes a requirements-based approach to software development. It begins with a clear and unambiguous definition of software requirements.
    • Objective: The objective is to establish a solid foundation for software development by specifying what the software should do, ensuring that developers have a clear understanding of the system’s operational requirements.
  3. Traceability:
    • Principle: Traceability is a central principle of DO-178B. It requires that each requirement be traced throughout the software development process, from design and coding to testing and verification.
    • Objective: Traceability ensures that every software requirement is addressed and validated, helping to guarantee that the software meets its intended objectives.
  4. Lifecycle Considerations:
    • Principle: DO-178B addresses the entire software development lifecycle, from requirements definition through design, coding, testing, verification, and validation.
    • Objective: The objective is to ensure that every phase of the development process is conducted rigorously and systematically, reducing the likelihood of errors or oversights.
  5. Safety Levels (A to E):
    • Principle: DO-178B classifies software into different safety levels (A, B, C, D, and E) based on the potential consequences of failure. The higher the safety level, the more stringent the requirements.
    • Objective: The objective is to tailor the level of scrutiny and testing to the criticality of the software, ensuring that the most critical software undergoes the most rigorous certification process.
  6. Certification Process:
    • Principle: DO-178B outlines a certification process that involves demonstrating that the software meets its intended objectives, is free from critical errors, and has been thoroughly tested.
    • Objective: The objective is to obtain certification from aviation authorities and regulators, such as the FAA or EASA, ensuring that the software complies with industry standards and safety regulations.
  7. Documentation and Records:
    • Principle: Comprehensive documentation and records are essential in DO-178B. Developers are required to maintain detailed records of the software development process.
    • Objective: The objective is to provide transparency and evidence of compliance with the standard, facilitating audits and inspections by certification authorities.
  8. Configuration Management:
    • Principle: DO-178B emphasizes configuration management, ensuring that software versions are controlled and that changes are tracked and validated.
    • Objective: The objective is to prevent unintended changes to the software and maintain the integrity of the certified system.

What is the difference between DO-178B and DO-178C?

DO-178B and DO-178C are both standards used in the aviation industry to ensure the safety and reliability of software in airborne systems, but there are some key differences between them:

  1. Publication and Revision:
    • DO-178B: Published in 1992, DO-178B was the second iteration of the DO-178 standard. It became widely adopted and established a set of guidelines for software development in airborne systems.
    • DO-178C: Published in 2011, DO-178C is the most recent version of the standard. It represents an evolution and improvement over DO-178B, addressing some of its limitations and incorporating modern software development practices.
  2. Development Process Models:
    • DO-178B: It primarily focuses on the Waterfall software development process model. The standard was created at a time when Waterfall was the dominant development approach.
    • DO-178C: DO-178C is more flexible in its approach to development process models. It recognizes that other development models, such as Agile and Iterative, are becoming more prevalent in the aviation industry. It provides guidance on how to adapt these models to meet the standard’s objectives.
  3. Tool Qualification:
    • DO-178B: The standard has relatively limited guidance on tool qualification, and the process for qualifying development tools is not as well-defined.
    • DO-178C: It provides more comprehensive guidance on tool qualification, reflecting the increased importance of software development tools in modern aviation software development.
  4. Object-Oriented Technology:
    • DO-178B: DO-178B does not provide explicit guidance on the use of object-oriented technology, which has become more prevalent in software development since its publication.
    • DO-178C: DO-178C includes guidance on using object-oriented technology, acknowledging its relevance, and providing criteria for its safe use in aviation software.
  5. Formal Methods:
    • DO-178B: While DO-178B mentions formal methods, it does not provide extensive guidance on their use.
    • DO-178C: DO-178C provides more detailed guidance on the use of formal methods, recognizing their potential benefits in ensuring software correctness and safety.
  6. Integration with Other Standards:
    • DO-178B: DO-178B can be challenging to integrate with other related standards, leading to potential inconsistencies and complexities in certification efforts.
    • DO-178C: DO-178C is designed to be more compatible with other aviation and safety standards, making it easier to integrate with complementary standards like DO-254 (hardware) and ARP4754A (systems).

Overall, DO-178C is an updated and more adaptable version of the standard, addressing shortcomings in DO-178B and providing clearer guidance on modern software development practices. It recognizes the evolving landscape of aviation software development and aims to improve safety and efficiency in the certification process.

Software Levels and Safety Levels of DO-178B

DO-178B describes five failure conditions, which are categorized by their effect on passengers, crew, and aircraft. Their effects are used to determine the Software Level, also known as the Design Assurance Level (DAL) or Item Development Assurance Level (IDAL). Software Level indicates the amount of effort that goes into the development of the given software application.

  • Level A (Catastrophic) – Failure prevents continued safe flight because it may cause a crash by disabling a critical function required to safely fly and land an aircraft.
  • Level B (Hazardous) – Failure has adverse effects on occupants because it reduces the ability of the operators to operate the aircraft properly. Serious or fatal injuries may occur.
  • Level C (Major) – Failure doesn’t have such a large impact as a Hazardous failure, but it’s still very significant and greatly increases the workload of the operators and reduces the margin in safety.
  • Level D (Minor) – Failure doesn’t have such a large impact as a major failure, but it’s still noticeable and may cause passenger inconvenience or a routine flight plan change.
  • Level E (No Effect) – Failure doesn’t affect operation capability at all and thus has no impact on the safety of aircraft or the workload of operators.

Reliable data on the costs associated with moving to a higher level are scarce, but the little data that are available point to an increase in development costs between 75% and 150%. The increase is caused largely by the increasing objectives to be met for each criticality level. DO-178B allows a great deal of flexibility when it comes to software development because of its objective-based nature since there are many possible ways for a real project to satisfy them.

Medical Device Risk Management

A generic DO-178B process is divided into five distinct processes, with each process having a set of expected documented outputs:

  • Software Planning – This is a description of the software development processes and the software lifecycle that will be used to satisfy the requirements of DO-178B. The output documents include a software development plan (SDP).
  • Development – This is a description of the software development processes and the software life cycle that is used to satisfy DO-178C objectives. The output documents include software requirements data (SRD), software design description (SDD), source code, and executable object code.
  • Verification – This is a description of the verification processes (Reviews, Analyses, and Tests) used to satisfy DO-178C objectives. The output documents include software verification cases and procedures (SVCP), and software verification results (SVR) with the review of all requirements, design, and code.
  • Configuration Management – This is a description of the methods and environment that will be used to configure all of the design data and compliance evidence needed to achieve DO-178C certification. The output documents include the software configuration index (SCI), and software life cycle environment configuration index (SECI).
  • Quality Assurance – This is a description of the methods and associated records that will be used to ensure that DO-178C quality assurance objectives are satisfied. The output documents include software quality assurance records (SQAR), software conformity review (SCR), and software accomplishment summary (SAS).

Scope and Applicability of DO-178B

DO-178B, formally known as “Software Considerations in Airborne Systems and Equipment Certification,” outlines specific guidelines and criteria for the development and certification of software used in airborne systems and equipment. The scope and applicability of DO-178B are defined to ensure the safety and reliability of software in the aviation industry. Here’s a detailed explanation of its scope and applicability:

  1. Aerospace Systems: DO-178B is primarily applicable to aerospace systems, including commercial and general aviation, as well as military aircraft. It covers a wide range of airborne systems, such as avionics, flight control systems, navigation systems, communication systems, and more.
  2. Safety-Critical Software: The standard is particularly focused on software that is safety-critical, meaning that its failure or malfunction could lead to catastrophic consequences, including loss of life, injury, or significant damage to the aircraft. It ensures that such software operates correctly and safely.
  3. Embedded Software: DO-178B is concerned with embedded software, which is software that is an integral part of an airborne system or equipment. This includes both real-time and non-real-time software components.
  4. Civil Aviation Regulation: The standard is designed to align with the regulations and guidelines set forth by aviation authorities and regulators, such as the Federal Aviation Administration (FAA) in the United States and the European Union Aviation Safety Agency (EASA) in Europe. Compliance with DO-178B is often a prerequisite for obtaining certification from these authorities.
  5. Development and Certification Process: DO-178B provides guidance on the entire software development lifecycle, from initial requirements through design, coding, testing, verification, and validation. It also outlines the certification process, which involves demonstrating that the software meets its intended safety and performance objectives.
  6. Safety Levels: DO-178B defines different levels of software criticality, ranging from Level A (most critical) to Level E (least critical). The specific safety level is determined by the potential consequences of software failure. Each safety level has corresponding requirements and guidelines for development and certification.
  7. Documentation and Traceability: The standard places a strong emphasis on documentation and traceability. Developers must maintain comprehensive records that demonstrate how software requirements are linked to design, code, and test cases. This ensures that every requirement is addressed and tested.
  8. Environmental Considerations: DO-178B takes into account the environmental conditions in which the airborne system will operate. It considers factors such as temperature, pressure, humidity, and electromagnetic interference, as these can affect the software’s performance and reliability.
  9. Safety Assurance: The primary goal of DO-178B is to provide safety assurance. It ensures that the software’s behavior under normal and abnormal conditions is well-understood, predictable, and safe. This is achieved through rigorous testing, analysis, and verification processes.
  10. Upgrades and Modifications: DO-178B also covers software upgrades and modifications. When changes are made to existing software, they must undergo a certification process to ensure that they do not compromise safety or reliability.

Risk Management in DO-178B

Risk management in DO-178B, also known as “Software Considerations in Airborne Systems and Equipment Certification,” is a critical aspect of the software development process for avionics systems. DO-178B is a set of guidelines and standards developed by the Radio Technical Commission for Aeronautics (RTCA) to ensure the safety, reliability, and certification of software used in civil aviation. Risk management within DO-178B is a systematic approach to identifying, assessing, and mitigating risks associated with avionics software development. Here’s a more detailed explanation of risk management in DO-178B:

1. Risk Identification:

  • The first step in risk management is identifying potential risks associated with the avionics software development process. This involves examining various aspects, including software requirements, design, coding, and testing.
  • Risks can stem from a variety of sources, such as unclear or ambiguous requirements, software complexity, inadequate testing, or hardware dependencies.

2. Risk Assessment:

  • Once risks are identified, they are assessed to determine their severity and likelihood. DO-178B categorizes risks into different levels or categories based on their potential impact on safety.
  • High-impact risks with a high probability of occurrence are considered more critical and require greater attention.

3. Risk Mitigation:

  • Risk mitigation involves implementing measures to reduce or eliminate identified risks. DO-178B provides guidelines for various software development processes to ensure that risks are addressed throughout the development lifecycle.
  • Strategies for risk mitigation may include redundancy, fault tolerance, error detection mechanisms, or changes in the software design.

4. Verification and Validation:

  • A fundamental aspect of DO-178B risk management is rigorous verification and validation. Software must undergo thorough testing and analysis to ensure it meets its intended functionality and safety objectives.
  • Verification activities include requirements-based testing, structural coverage analysis, and fault injection testing, among others. These activities help confirm that the software behaves as expected and is free from critical errors.

5. Documentation:

  • DO-178B places a strong emphasis on documentation. Detailed records must be maintained throughout the software development process to demonstrate compliance with safety and certification requirements.
  • Documentation includes design decisions, test cases, test results, and verification activities. Proper documentation ensures transparency and traceability.

6. Independence and Reviews:

  • DO-178B emphasizes independence in the verification and validation processes. Independent verification teams are responsible for reviewing and evaluating the software to ensure it meets safety objectives.
  • Independent assessments help identify and rectify potential risks and issues. This independence adds another layer of scrutiny to the software development process.

7. Continuous Monitoring:

  • Risk management in DO-178B is not a one-time activity but an ongoing process. Risks are continually monitored throughout the software development lifecycle.
  • As the development progresses, new risks may emerge, and existing risks may evolve. It is essential to adapt risk mitigation strategies accordingly.

8. Compliance with Certification Requirements:

  • One of the primary objectives of DO-178B is to ensure that avionics software meets certification requirements set by aviation authorities. Effective risk management is critical for demonstrating compliance with these requirements.

In summary, risk management in DO-178B is a comprehensive and systematic approach to identifying, assessing, and mitigating risks associated with avionics software development. It is crucial for ensuring the safety, reliability, and certification of software used in civil aviation, where the consequences of software failures can be catastrophic. By following DO-178B risk management practices, aviation companies can enhance the safety and quality of their software systems while meeting regulatory and certification standards.

Certification and Compliance of DO-178B

Certification and compliance with DO-178B, formally known as “Software Considerations in Airborne Systems and Equipment Certification,” are critical aspects of ensuring that software used in airborne systems meets the necessary safety and reliability standards. Certification is a formal process that involves obtaining approval from aviation authorities or regulatory bodies, such as the Federal Aviation Administration (FAA) in the United States or the European Union Aviation Safety Agency (EASA) in Europe. Here’s an explanation of the certification and compliance process for DO-178B:

  1. Determination of Safety Level:
    • Before initiating the certification process, it is essential to determine the safety level (Level A, B, C, D, or E) that corresponds to the software being developed. The safety level is determined based on the potential consequences of software failure.
  2. Compliance Planning:
    • Establish a compliance plan that outlines how the software development process will align with DO-178B requirements. This plan includes the identification of objectives, tasks, and responsibilities related to software development and certification.
  3. Requirements Compliance:
    • Ensure that software requirements are clearly defined and traceable. Each software requirement must be traceable to system-level requirements and have corresponding design, code, and test cases.
    • Verification activities, such as reviews, inspections, and testing, are conducted to confirm that software requirements are met.
  4. Design and Code Compliance:
    • Develop a detailed software design that reflects the high-level software requirements. The design should be traceable to the requirements.
    • Code the software according to the design and ensure that the code is traceable to both the design and requirements.
    • Perform reviews, inspections, and testing to verify that the design and code comply with DO-178B objectives and safety requirements.
  5. Verification and Validation:
    • Verification activities include static analysis, dynamic testing, and other techniques to ensure that the software operates correctly and safely.
    • Validation activities involve testing the software in a real or simulated environment to demonstrate that it performs its intended functions under various conditions.
  6. Documentation and Records:
    • Maintain comprehensive documentation and records throughout the software development process. These records provide evidence of compliance with DO-178B and are subject to scrutiny during certification audits.
    • Documentation includes requirements specifications, design documents, code reviews, test plans, test cases, test results, and configuration management records.
  7. Traceability:
    • Ensure that traceability is maintained throughout the development process. Traceability matrices demonstrate the relationships between requirements, design, code, and test cases, ensuring that all requirements are addressed and validated.
  8. Configuration Management:
    • Implement configuration management practices to control software versions and changes. Configuration management helps prevent unauthorized modifications and ensures that the certified software remains unchanged during operation.
  9. Certification Support:
    • Prepare a certification package that includes all relevant documentation, records, and evidence of compliance with DO-178B.
    • Engage with aviation authorities or regulatory bodies to undergo the formal certification process. This involves submitting the certification package and participating in audits and reviews.
  10. Audit and Approval:
    • Aviation authorities review the certification package, conduct audits, and assess compliance with DO-178B.
    • Once the software is deemed compliant and safe, the authorities grant certification, allowing the software to be used in airborne systems.
  11. Post-Certification:
    • Even after certification, ongoing compliance is essential. Any modifications or updates to the software must undergo recertification to ensure that they do not compromise safety or reliability.

Certification and compliance with DO-178B are essential to ensure that software in airborne systems meets the highest safety standards. It is a rigorous and meticulous process that requires careful planning, documentation, and verification to achieve successful certification and ensure the safe operation of aviation systems.

Challenges and Criticisms of DO-178B

While DO-178B has been a widely adopted and effective standard for ensuring the safety and reliability of software in airborne systems, it is not without its challenges and criticisms. Here are some of the common challenges and criticisms associated with DO-178B:

  1. Rigidity and Prescriptiveness:
    • Challenge: DO-178B is often criticized for being rigid and overly prescriptive, especially when compared to more modern software development methodologies like Agile. Its waterfall-style approach can be seen as inflexible.
    • Criticism: Critics argue that the standard may not easily accommodate rapid changes or evolving requirements in software development.
  2. High Costs and Resource Intensiveness:
    • Challenge: Achieving compliance with DO-178B can be resource-intensive and costly. It requires extensive documentation, testing, and verification efforts.
    • Criticism: Smaller companies, startups, or projects with limited budgets may find it challenging to meet the standard’s requirements.
  3. Complexity of Certification:
    • Challenge: The certification process for DO-178B can be complex and time-consuming. It involves interactions with aviation authorities and regulatory bodies, which can slow down the development and deployment of aviation systems.
    • Criticism: Some argue that the certification process could be streamlined and made more efficient.
  4. Limited Guidance on Modern Practices:
    • Challenge: DO-178B was developed at a time when traditional waterfall development was the norm. It provides limited guidance on how to adapt to modern software development practices, such as Agile and DevOps.
    • Criticism: Critics contend that the standard should provide more explicit guidance on how to apply these practices while ensuring safety.
  5. Object-Oriented Programming (OOP):
    • Challenge: DO-178B does not provide extensive guidance on using object-oriented programming (OOP), which is a common approach in modern software development.
    • Criticism: Incorporating OOP can be challenging within the framework of DO-178B, and developers may need to make additional efforts to demonstrate compliance.
  6. Formal Methods:
    • Challenge: While DO-178B mentions formal methods, it does not provide detailed guidance on their use. Formal methods can be valuable for ensuring software correctness and safety.
    • Criticism: Critics argue that the standard should offer more comprehensive support for the use of formal methods.
  7. Interactions with Other Standards:
    • Challenge: Integrating DO-178B with other aviation-related standards, such as DO-254 (hardware) and ARP4754A (systems), can be complex and challenging, leading to potential inconsistencies.
    • Criticism: Some argue that greater harmonization and consistency among these standards could benefit the industry.
  8. Adaptation to New Technologies:
    • Challenge: DO-178B was developed before the proliferation of certain technologies, like modern multicore processors and advanced sensors. Adapting the standard to these technologies can be difficult.
    • Criticism: Critics suggest that the standard needs to be updated to address the challenges posed by new and emerging technologies.

It’s important to note that many of these challenges and criticisms have been addressed in the subsequent version, DO-178C, which was developed to be more adaptable to modern development practices and technologies. However, DO-178B still has a significant legacy presence in the aviation industry, and these challenges may persist in projects that continue to rely on it.

Modern Practices and Technologies for DO-178B

DO-178B, while developed during a time when traditional waterfall development practices were dominant, can still be adapted to accommodate modern software development practices and technologies to some extent. Here’s an explanation of how modern practices and technologies can be integrated into a DO-178B-complaint process:

  1. Agile Methodologies:
    • Explanation: Agile methodologies, such as Scrum or Kanban, are increasingly being adopted in software development to promote flexibility and responsiveness to changing requirements.
    • Integration with DO-178B: While DO-178B’s traditional approach is more sequential, it is possible to adapt some Agile principles to the process. For instance, requirements can be managed in smaller, iterative increments, with regular reviews and testing conducted at each iteration.
  2. DevOps Practices:
    • Explanation: DevOps combines development and operations, emphasizing automation, continuous integration, and continuous delivery (CI/CD) to accelerate software development and deployment.
    • Integration with DO-178B: Automation can be employed in testing and verification processes, ensuring that each code change is thoroughly tested as part of the CI/CD pipeline. This can improve efficiency while still adhering to DO-178B’s verification requirements.
  3. Object-Oriented Programming (OOP):
    • Explanation: OOP is a widely used paradigm in modern software development, enabling modular and maintainable code.
    • Integration with DO-178B: While DO-178B may not explicitly address OOP, you can still use OOP principles in software design and development. Ensure that your design and code are well-documented, and that traceability is maintained between OOP constructs and requirements.
  4. Formal Methods:
    • Explanation: Formal methods involve mathematical techniques for proving the correctness of software. They are valuable for critical systems where safety and reliability are paramount.
    • Integration with DO-178B: DO-178B mentions the use of formal methods, and DO-178C provides more guidance on their use. You can apply formal methods to critical portions of the codebase to ensure correctness, safety, and reliability.
  5. Model-Based Development (MBD):
    • Explanation: MBD uses graphical models as a foundation for software development, making it easier to visualize and understand complex systems.
    • Integration with DO-178B: You can use MBD tools and techniques for requirements modeling, system design, and simulation. Ensure that models are well-documented and traceable to the final code.
  6. Testing and Test Automation:
    • Explanation: Modern testing practices, including automated unit testing, integration testing, and regression testing, can improve software quality and reliability.
    • Integration with DO-178B: Implement automated testing frameworks to efficiently conduct unit testing, integration testing, and other required tests. Automation can help ensure that all requirements are thoroughly verified.
  7. Risk-Based Approach:
    • Explanation: A risk-based approach involves identifying and prioritizing the most critical aspects of software development and testing based on potential impact and likelihood.
    • Integration with DO-178B: Use a risk-based approach to focus verification efforts on the most critical software components. This can help allocate resources more effectively and ensure that safety-critical aspects receive the highest scrutiny.
  8. Multicore Processors and Parallelism:
    • Explanation: Modern avionics systems often include multicore processors and parallel computing to enhance performance.
    • Integration with DO-178B: Adapting DO-178B to multicore processors requires careful consideration of safety and reliability aspects, including managing shared resources and ensuring determinism in real-time systems.
  9. Open Source and Commercial Tools:
    • Explanation: Leveraging open-source and commercial development tools and libraries can improve development efficiency and maintainability.
    • Integration with DO-178B: When using such tools, ensure that they are qualified and documented according to DO-178B requirements, including tool qualification processes.

Incorporating modern practices and technologies into a DO-178B-compliant process requires a careful balance between agility, safety, and rigorous documentation and verification. Customizing the approach to suit the specific needs and constraints of the project is crucial to achieving the desired level of safety and reliability while benefiting from modern software development advancements.

Documentation Required for DO-178B

There are several documents required for DO-178B compliance. They include:

  • Plan for Software Aspects of Certification (PSAC)
  • Software Quality Assurance Plan
  • Software Configuration Management Plan
  • Configuration Control Procedures
  • Software Code Standard
  • Software Design Standard
  • Software Requirements Standard
  • Software Development Plan
  • Software Verification Plan
  • Source, Executable Object Code, SCI and SECI
  • Software Design Document
  • Software Requirements Document
  • Traceability
  • Test Cases and Procedures
  • Verification Results
  • Quality Assurance Records
  • Configuration Management Records
  • Problem Reports
  • Software Accomplishments Summary

Supporting the DO-178B with a Requirement Management Tool

Visure Solutions is a software company that specializes in providing requirements and risk management solutions, including those tailored to the aerospace industry’s specific needs, such as compliance with DO-178B. Visure Solutions offers tools and services that help organizations manage the complex requirements, risk assessment, and compliance processes associated with DO-178B. Here’s how Visure Solutions addresses DO-178B compliance, along with insights into their AI integration and risk management capabilities:

DO-178B Compliance with Visure Solutions:

  1. Requirements Management:
    • Visure Solutions provides a comprehensive platform for managing requirements, a critical aspect of DO-178B compliance. Their platform allows aerospace companies to define, trace, and maintain software requirements, ensuring complete coverage and traceability throughout the software development lifecycle.
  2. Traceability and Impact Analysis:
    • The Visure Solutions platform supports bidirectional traceability, enabling organizations to establish and maintain trace links between requirements, design, and verification activities. This is essential for demonstrating compliance with DO-178B’s stringent traceability requirements.
  3. Change Management:
    • Change management is crucial in DO-178B, as any modifications to requirements or design must be rigorously assessed for their impact on safety and compliance. Visure Solutions’ tools facilitate change management by tracking and managing changes to requirements and associated artifacts.
  4. Verification and Validation:
    • Visure Solutions’ platform supports verification and validation activities, helping organizations create and manage test cases, track test results, and ensure that verification activities align with DO-178B objectives.

AI Integration:

Visure Solutions has incorporated AI and machine learning capabilities into its platform to enhance requirements and risk management processes:

  1. Intelligent Analytics:
    • AI-driven analytics can help identify potential issues or risks within requirements and design documents. For example, machine learning algorithms can flag inconsistencies, ambiguities, or missing information in requirements, allowing teams to address them proactively.
  2. Automated Traceability:
    • AI can assist in automating the traceability process by suggesting potential trace links based on the historical data and patterns it has learned. This streamlines the often complex and time-consuming task of maintaining traceability matrices.
  3. Predictive Risk Assessment:
    • AI can be used to analyze historical project data and identify patterns related to risk factors. This enables organizations to proactively identify and mitigate risks that might otherwise go unnoticed until later in the development process.

Risk Management with Visure Solutions:

  1. Risk Identification and Assessment:
    • Visure Solutions’ platform includes features for risk identification and assessment. Users can define and categorize risks, assign risk owners, and assess their potential impact and likelihood, aligning with DO-178B’s risk management requirements.
  2. Risk Mitigation and Monitoring:
    • The platform supports risk mitigation by allowing organizations to define and track risk mitigation plans and actions. Automated alerts and notifications can ensure that mitigation efforts stay on track.
  3. Traceability to Risks:
    • Visure Solutions enables traceability between risks and related requirements, design elements, and verification activities. This ensures that risks are adequately addressed throughout the development process.
  4. Documentation and Reporting:
    • The platform provides tools for documenting risk management activities and generating reports for regulatory compliance and audit purposes. This documentation is crucial for demonstrating adherence to DO-178B’s risk management guidelines.

In conclusion, Visure Solutions offers a comprehensive suite of tools and capabilities for organizations in the aerospace industry seeking to achieve DO-178B compliance, manage requirements effectively, integrate AI-driven insights into their processes, and implement robust risk management practices. By leveraging Visure Solutions’ solutions, aerospace companies can enhance the quality, safety, and compliance of their avionics software while streamlining their development and certification processes.


DO-178B is a software standard that ensures safety-critical software is designed, developed, and tested in a consistent and repeatable manner. The standard has been around since the early 1990s and has been updated over time to account for changes in technology. Many commercial aviation organizations require their suppliers to be certified to DO-178B as part of doing business with them. In order to achieve certification, organizations must go through a rigorous process that includes documenting all aspects of the software development lifecycle. Visure Requirements ALM Platform is one of the few requirements management tools that has been certified to support DO-178B at Level A, the highest level of certification. If you are looking for an end-to-end solution for managing your requirements and want to ensure compliance with this important standard, give Visure Requirements a try today. Try out the Free 30-day Trial Now!

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IBM Rational Doors Software

The High Cost of Poor Requirements Management

June 06th, 2024

11 am EST | 5 pm CET | 8 am PST

Louis Arduin

Louis Arduin

Main Speaker

Impact & Solutions for Inefficient Requirements Management

Explore the significant impact that inefficient requirements management practices can have on project costs and timelines.