The term that is being used to call the electronic systems that are commonly being used on spacecraft, artificial satellites, and aircraft, is avionics. Some of the inclusions for this particular electronic system include the management, display, navigation, and communications of multiple systems and the term avionics is actually derived from the words electronics and aviation. The avionics equipment can be found usually in the cockpit of an aircraft, including the other systems such as anti-collision systems, control, monitoring, communication, weather, and navigation.
The so-called embedded software that is commonly being used in avionics is typically called as avionics software and it basically contains safety and reliability concerns that are legally mandated.
The standard guidelines for the process of developing and producing the system of the avionics software are the DO-178 and it typically deals with the safety of the software that is developed as safety-critical designed specifically for the various airborne systems. To be more specific, the DO-178 is actually a guideline that is basically with the title as software considerations in airborne systems and equipment certification, but it is commonly referred by the aviation industry as the bible of avionics software development.
This particular guideline has similarities with the standards that are being used for nuclear power, military aviation, medical devices, automotive, and railroads. In this day and age, the DO-178 is evolving into three subsequent iterations, and it basically provides the avionics industry with a successful framework in which the avionic software developers and the certification authorities may work with full vision. The three integral processes that are being used in do 178b typically start with the planning process, and once the planning process is complete the development process will follow, while the last and the largest process of all, is the correctness or the integral processes.Find the best do-254 certification services.
The planning process includes the SVP which stands for software verification plan, the PSAC which stands for the plan for software aspects of certification, the SQAP which stands for software quality assurance plan, the SDP which stands for the software development plan, and the SCMP which stands for software configuration management plan. The three primary standards that are being used in DO-178 include software coding standards, software requirements standards, and software design standards. The testing for DO-178, such as the functional testing, is actually based upon requirements, and there are actually five criticality levels for this particular guideline and it basically calls for more software testing that is significant as the level of criticality is increasing. You can read more on this here: https://en.wikipedia.org/wiki/Avionics_software.
