Design of Long-Endurance Systems With Inherent Robustness to Partial Failures During Operations

This article presents an integrated multistate method for the early-phase design of inherently robust systems; namely, those capable, as a prima facie quality, of maintaining adequate performance in the face of probabilistic system events or failures. The methodology merges integrated multidisciplinary analysis techniques for system design with behavioral-Markov analysis methods used to define probabilistic metrics such as reliability and availability. The result is a multistate approach that concurrently manipulates design variables and component failure rates to better identify key features for an inherently robust system. This methodology is demonstrated on the design of a long-endurance unmanned aerial vehicle for a three-month ice surveillance mission over Antarctica. The vehicle is designed using the multistate methodology and then compared to a baseline design created for the best performance under nominal conditions. Results demonstrated an improvement of 10–11% in system availability over this period with minimal impacts on cost or performance.

[1]  P. S. Babcock,et al.  An automated environment for optimizing fault-tolerant systems designs , 1991, Annual Reliability and Maintainability Symposium. 1991 Proceedings.

[2]  Jan Roskam Methods for Estimating Stability and Control Derivatives of Conventional Subsonic Airplanes , 1971 .

[3]  Sergei Utyuzhnikov,et al.  Control of robust design in multiobjective optimization under uncertainties , 2012 .

[4]  Karl Iagnemma,et al.  Reconfigurability in planetary surface vehicles : Modelling approaches and case study , 2006 .

[5]  Iv P.S. Babcock Channelization: the two-fault tolerant attitude control function for the Space Station Freedom , 1996 .

[6]  Richard E. Barlow,et al.  Coherent Systems with Multi-State Components , 1978, Math. Oper. Res..

[7]  Martin Spieck,et al.  MDO: assessment and direction for advancement—an opinion of one international group , 2009 .

[8]  D. Elmakis,et al.  Power system structure optimization subject to reliability constraints , 1996 .

[9]  Michel D. Ingham,et al.  Application of State Analysis and Goal-Based Operations to a MER Mission Scenario , 2006 .

[10]  Kelly Cohen,et al.  First Order Effects of New Technology on a High Altitude Long Endurance (HALE) Unmanned Aerial Vehicle (UAV) , 2008 .

[11]  Adamantios Mettas,et al.  Reliability allocation and optimization for complex systems , 2000, Annual Reliability and Maintainability Symposium. 2000 Proceedings. International Symposium on Product Quality and Integrity (Cat. No.00CH37055).

[12]  Jack P. C. Kleijnen Design and Analysis of Simulation Experiments , 2007 .

[13]  Lisa L. Kohout,et al.  High Altitude Long Endurance Air Vehicle Analysis of Alternatives and Technology Requirements Development , 2007 .

[14]  Olivier L. de Weck,et al.  Multistate Design Approach to Analysis of Twin-Engine Aircraft Performance Robustness , 2012 .

[15]  David Penn,et al.  The CAPECON Program: Civil Applications and Economical Effectivity of Potential UAV Configurations , 2004 .

[16]  Masahiro Ono,et al.  A Probabilistic Particle-Control Approximation of Chance-Constrained Stochastic Predictive Control , 2010, IEEE Transactions on Robotics.

[17]  Tapabrata Ray,et al.  Practical Robust Design Optimization Using Evolutionary Algorithms , 2011 .

[18]  Richard M. Murray,et al.  Safety verification of a fault tolerant reconfigurable autonomous goal-based robotic control system , 2007, 2007 IEEE/RSJ International Conference on Intelligent Robots and Systems.

[19]  Gregory Levitin,et al.  Multi-State System Reliability - Assessment, Optimization and Applications , 2003, Series on Quality, Reliability and Engineering Statistics.

[20]  Alejandro D. Domínguez-García,et al.  An integrated methodology for the dynamic performance and reliability evaluation of fault-tolerant systems , 2008, Reliab. Eng. Syst. Saf..

[21]  Y. Massim,et al.  Optimal Design and Reliability Evaluation of Multi-State Series-Parallel Power Systems , 2005 .

[22]  Gregory Levitin,et al.  A new approach to solving problems of multi‐state system reliability optimization , 2001 .

[23]  Igor Ushakov The method of generalized generating sequences , 2000, Eur. J. Oper. Res..

[24]  M. Smotherman,et al.  A non-homogeneous Markov model for phased-mission reliability analysis , 1989 .

[25]  David W. Coit,et al.  MOMS-GA: A Multi-Objective Multi-State Genetic Algorithm for System Reliability Optimization Design Problems , 2008, IEEE Transactions on Reliability.

[26]  David G. Ward,et al.  System Identification for Retrofit Reconfigurable Control of an F/A-18 Aircraft , 2005 .

[27]  Daniel P. Raymer,et al.  Aircraft Design: A Conceptual Approach , 1989 .

[28]  Peter J. Haas,et al.  Stochastic Petri Nets: Modelling, Stability, Simulation , 2002 .