DEVELOPMENT OF OPERATING CONCEPTS

T.E. (Ted) Thompson
Transport Canada Aviation
320 Queen Street, AANFD
Ottawa, Ontario, Canada K1A 0N8


Abstract. Systems engineering techniques, especially requirements collection and management, are well described in the literature but appropriate methods of determining and documenting operator requirements are not as widely discussed. The Canadian Airspace System (CAS) is a large, complex systems engineering task. This paper discusses the methods used by Transport Canada to elicit, review, discuss and document the operating concepts for the future evolution of the CAS.

CONTEXT

The Canadian Airspace System (CAS) is the collection of equipment and facilities which, together with skilled people, processes and procedures, makes up the Air Navigation System which ensures the safe conduct of air traffic in Canada.

 Noteworthy aspects of the CAS include its;

     
  1. size (over 30,000 systems serving 2,000 operators),
  2. diversity (several hundred subsystem procurement and installation projects over many years),
  3. geographic scale (1.5 billion hectares from the Pacific coast to the mid-Atlantic and from the Great Lakes to the North Pole),
  4. scope (2,000 sites across Canada including 58 towers, 102 Flight Service Stations, 2 Terminal Control Units, and 7 Area Control Centres plus several regional and national facilities),
  5. time scale (to the year 2005 and beyond),
  6. cost (expected to exceed $4 Billion by 2000),
  7. diverse communications requirements (voice, data, navigation, fixed, mobile, far north, mid-ocean),
  8. large user community with varying requirements for levels of service.
The CAS is without doubt a large and complex system and the application of system engineering principles is absolutely necessary to avoid expensive duplication or incompatibilities in implementing the many subsystems. In the past, subsystems were simpler and were relatively stand-alone. Today's systems are so complex that it has become very difficult to be sure that the final system is correct and is neither over- nor under-specified.

 In 1989, the Canadian Government Department of Transport embarked on a System Engineering and Integration Project to formalize the processes for the definition of requirements and the evolution of the system design of the CAS. As air navigation is a continuing business, a "clean-sheet" design is not possible. Every design decision flows to some extent from today's system in an evolutionary rather than revolutionary manner.

 Transport Canada uses the normal sequence of system engineering steps shown in Figure 1:
 
 

  1. Understand mission needs

  2. [System Engineering Flow Diagram]
  3. Develop the operating concepts

  4.  
  5. Specify system requirements

  6.  
  7. Specify the system design

  8.  
  9. Develop a transition plan
A key component is the database of system level requirements, including the traceability to higher level requirements. The system documentation is only a snapshot of the database at some point in time. The "real" system design is the database itself; the documentation is produced to facilitate review and discussion.

Much has been published on the development and maintenance of large requirements databases but there has been little discussion on the derivation of those requirements. In this paper I will concentrate on step 2 in the standard process - the techniques we use to develop and maintain the operating concepts.
 
 

UNDERSTAND MISSION NEEDS

This is the highest level definition of the needs of the users (the aviation community) reflecting the policies of the service provider (the Federal Government of Canada). Services are based on the pilots' needs, international aviation commitments and government policies. There are only 28 services at this level and each is directly traceable to Government policy or to an Act of Parliament. The formal document is known as the Operations Requirement Document.

 A very structured format was chosen to document ANS services. Each is stated in the form: "The air navigation system shall..." which helps ensure that it is written from the point of view of a user who is outside the system. Each statement is a concise, single sentence describing the "what" of a system service followed by the precise but high-level details of that service. An example is:

 "The ANS shall provide to user aircraft in flight a volume of conflict free airspace."

 The "how" is described later in the form of Operating Concepts.
 
 

THE CONCEPTS

Operating concepts must be developed to establish which system level processes and tasks will be accomplished by people or procedures and which will best be accomplished by the "machinery" of the CAS in support of the Mission Needs.

 The concept documents provide a system model which:
 
 

  1. describes the functional involvement of the operators and users of the system;
  2. defines the facilities and operational positions within those facilities from which services are to be provided;
  3. specifies the flow of information through the system in support of defined services from the source to the user of the data;
  4. allocates the data processing functions to either human or machine;
  5. reflects future technologies and demands and is readily revised as they evolve;
  6. represents a consensus among concerned operational, technical and user agencies;
  7. is based on and is fully traceable to the operations requirements document; and
  8. forms the basis for development of detailed system-level functional requirements.
Two documents were produced to describe operating concepts. One describes all aspects of the CAS related directly to the control of air traffic while the other describes all logistic support matters, such as maintenance, training and simulation, that support the operational concept.

 Both documents describe the relevant concepts from the point of view of the user expectations of the CAS. For each operating position (such as "Radar Controller" or "Maintenance Supervisor") every required function of the position is tabulated to describe the expected machine inputs and outputs. We must keep in mind, though, that the system design is targeted at 10 years in the future so the concepts describe the future work of the operators and users of the equipment, not the way it is done today.

 Where do these concepts come from? As the system we are defining will evolve from today's system, it is clear that many of the concepts will be based on today's concepts. A number of the concepts are defined for us by ICAO, the International Civil Aviation Organization.

 We also recognize that many concepts first appear as something an operator saw at a trade show or read about in a magazine. Proposed concepts are often driven by "what can now be done through technology" as much as by "what we really need to do".

A major task for the concept design team is to consider the various concept alternatives and to decide on the most efficient and cost effective options, including quantities and locations for various facilities.

 Concepts are evaluated through discussions with users and operators, operational simulations, formal task analysis and structured trade-off studies. All evaluation teams take pains to avoid describing hardware, software or product specific solutions. There is plenty of opportunity for that later.

 All the concepts treat the entire CAS as a single "black box" that is defined in terms of input and output. The precise algorithms for linking specific inputs and outputs are not described at this point, nor are the specific pieces of equipment or sub-systems.

 Similarly, the concept documents do not discuss the details of the Computer/Human Interface (CHI). It is important not to get mired in details such as the size of the window on the display or the colour of the characters or the switch at this time. Those are implementation details that are best determined through extensive human factors prototyping and testing in a simulated operational environment.
 
 

CONCEPT DOCUMENT CONTENTS

Section 1. The first section contains a description of the operating environment and its constraints on the operating concepts. Such issues as the type and extent of airspace served, the number and types of users, the distribution of aerodromes served and the planned types and locations of operational facilities are described and evaluated. All these factors constrain the range of possible design solutions.

 Section 2. The second section identifies those services to be provided by the system. Each service is as defined in the Operations Requirement Document and information is provided on to whom, by whom, and how the service may be provided. This section also describes any special technology that is to be employed as mandated by international agreement. The information is provided in an easily understood and concise textual form that requires only about one page per service.

 Section 3. The third section is broken into three parts, the context description, the system model and the operational scenarios. The first two parts use formal data flow graphical design and documentation techniques. The context diagrams define all the external entities that communicate or interact with the CAS while the system model describes staffed and unstaffed facilities, logical workstation positions and activities required to deliver the required services. This is the point at which it becomes essential to make use of efficient software tools for modelling the system and maintaining the data dictionary. All functions associated with each workstation are allocated to human, machine or procedure and tabulated for review. This tabulation defines implicitly where human/machine interfaces occur. These interfaces are tabulated separately in terms of form (text input, graphic display, alarm etc.), description and stimulus.

 The operational scenarios were devised to demonstrate the sequential flow of activities in the future ANS and provides an opportunity for the user and operator experts to validate the specific ideas expressed in the rest of Section 3. The scenarios are as detailed as possible and include, for example, references to specific airports and air routes to facilitate accurate visualization by the reviewers. The set of scenarios were crafted to exercise every facility and function and a cross reference table is included.

 Appendices. The concept document contains several appendices, the most important of which is the traceability matrix which is organised on a function by function basis to trace back to the high level service requirements. This information are not now required in paper form as good software requirements management tools enforce and manage requirements traceability.

 A second major appendix captures those future operating concepts that were known to be imminent but which were not adequately defined by international bodies for inclusion in the system design at this time. They will be re-evaluated and included as necessary at a later date.
 
 

CONCLUSION - LESSONS LEARNED

The concept documents form a solid basis for the further system design but the design team learned several valuable lessons from the development process.
 
 

BIOGRAPHY

Mr. Thompson worked with Transport Canada from 1971 when he received a BASc Degree in Computer Engineering from the University of Waterloo, Waterloo, Ontario, Canada until he left to pursue a consulting career in 1995. He received his MSc degree in Aviation Electronic Systems from the Cranfield Institute of Technology, Cranfield, England in 1980. As Chief Systems Engineer, he was responsible for the engineering development, technical system design and advanced project management tools and procedures for the transition from today's system to the future Canadian Airspace System.



 
© T. E. Thompson 2014
Thompson Aviation Transportation Systems
7075 Quinnfield Way, Greely, Ontario,
Canada K4P 1B7
telephone: + 1 613 574 2803

e-mail to: consult@thompsonats.com

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