Software development process for the Aviation Mission Planning System (AMPS): a case study
Edwards, Keith R.
McCaffrey, Martin J.
Marvel, Orin E.
MetadataShow full item record
The DoD software development environment is one in needed transition. Many of the old methodologies have been less than effective for software development. Emerging methods and techniques, for instance, evolutionary development and incremental delivery, and the use of CASE tools, are supported by a new set of flexible standards. MIL-STD-498, Software Development and Documentation. and the coming commercial equivalent, emphasize flexibility, tailoring, and value-added activities. The Aviation Mission Planning Systems (AMPS) software development effort, is a study in the employment of innovative, emerging methods and techniques in this evolving environment. Originally a prototype, the AMPS program will now lead to a production system. The development process for the supporting software is now undergoing a transition. This thesis examines this transition and discusses several process improvement considerations as they relate to the AMPS software development process. Additionally, this thesis explores several areas of concern surrounding the AMPS software development process transition, and suggests possible mitigation approaches.
Showing items related by title, author, creator and subject.
Naegle, Brad R. (Monterey, California. Naval Postgraduate School, 2017-04); NPS-CE-17-042Department of Defense (DoD) software-intensive systems and the software content in other systems will continue to grow and may dominate total ownership costs (TOC) in the future. These costs are exacerbated by the fact ...
Naegel, Brad R. (Monterey, California. Naval Postgraduate School, 2017-04-19); NPS-CE-17-042Department of Defense (DoD) software-intensive systems and the software content in other systems will continue to grow and may dominate total ownership costs (TOC) in the future. These costs are exacerbated by the fact ...
Development of a nonlinear 6-degree of freedom miniature rotary-wing unmanned aerial vehicle software model and PID flight path controller using Mathworks Simulink simulation environment Miranda, Ricardo E. (Monterey, California: Naval Postgraduate School, 2009-09);This paper describes the development of a 6-degree of freedom (6-DOF), nonlinear, miniature rotary-wing unmanned aerial vehicle (RW UAV) simulation environment using MathWorks Simulink simulation software. In addition ...