Military Embedded Systems Summer 2006

More documents

Recommendations

Info

Mil Tech Trends ID Description 1 Each actuator will have five modes: Isolated, Off, Passive, Standby, and Active. 2 If possible, the same control law should be active for both the left and right elevators. 3 If available, the I/O control law should be active instead of the DL control law. 4 The actuator that is not active should be in standby. 5 6 If the pressure of the hydraulic circuit is low and the position measurement fails, the corresponding actuator should be switched to Off. If the pressure of the hydraulic circuit is nominal and the position measurement fails, the corresponding actuator should be switched to Isolated. 7 Controller state changes should be made only in response to failure events. If one actuator can be operated only in DL, should the other still be operated in I/O? Therefore, it is necessary to test the detailed requirements early in the development process to ensure their accuracy. Tracing requirements to design Implementing the mode logic component as software requires translating the detailed requirements in Table 2 into an executable language such as C. Going directly to a programming language from the requirements, however, can leave too much room for interpretation. As a result, errors in the requirements or design may not be found until late in the development process, when subsystem and system integration is done, causing costly Table 1 2.1.1 Hydraulic pressure 1 failure If a failure is detected in the hydraulic pressure 1 system, while there are no other failures, isolate the fault by switching the left outer actuator to the Off mode. 2.1.2 Hydraulic pressure 1 fails and then recovers If a failure is detected in the hydraulic pressure 1 system and the system then recovers, switch the left outer actuator to the Standby mode. 2.1.3 Hydraulic pressure 2 failure If a failure is detected in the hydraulic pressure 2 system, while there are no other failures, isolate the fault by switching the left inner actuator and the right inner actuator to the Off mode. 2.1.4 Hydraulic pressure 2 fails and then recovers If a failure is detected in the hydraulic pressure 2 system and the system then recovers, switch the left inner actuator and the right inner actuator to the Standby mode. 2.1.5 Hydraulic pressure 3 failure If a failure is detected in the hydraulic pressure 3 system, while there are no other failures, isolate the fault by switching the right outer actuator to the Off mode. 2.1.6 Hydraulic pressure 3 fails and then recovers If a failure is detected in the hydraulic pressure 3 system and the system then recovers, switch the right outer actuator to the Standby mode. 2.2.1 Default start-up condition If there have been no failures detected, the outer actuators have priority over the inner actuators. Therefore, the elevator actuators should default to the following modes. The left outer and right outer actuators should transition from the Passive mode to the Active mode. The left inner and right inner actuators should transition from the Passive mode to the Standby mode. 36 / SUMMER <strong>2006</strong> <strong>Military</strong> EMBEDDED SYSTEMS Table 2
HE104+DX Mil Tech Trends design iterations. Instead, modeling the design in a higher-level language, such as Simulink and Stateflow from The MathWorks, facilitates understanding of the design through simulation, so that system interactions can be studied much earlier. C code can then be automatically generated from the model, eliminating manual coding errors. In constructing the design model, detailed requirements can be associated with elements in the model by using Simulink Verification and Validation. This association provides requirements traceability, which helps ensure that all the requirements have been incorporated into the design early in the development process. Flash Solutions DiskOnChip family of products Standard interfaces, including 32 pin DIP, UBS and IDE Multiple capacities (16MB - 1GB) Advanced Error Correction 108 Watt PC/104+ Power Supply 108 Watt High Efficiency Power Supply +3.3V, +5V, +12V and -12V DC output 6V to 40V DC input range Extended temperature: -40 O C to +85 O C PC/104-Plus to Mini PCI Adapter AD006 Compatible with standard Universal, 3.3V or 5V PC/104-Plus stack Mini PCI Type III 124 pin female socket PC/104-Plus 120 pin stack-through connector Extended temperature: -40°C to 85°C RSC# 3701 @www.mil-embedded.com/rsc www.tri-m.com info@tri-m.com 1.800.665.5600 HEAD OFFICE: VANCOUVER tel: 604.945.9565 fax: 604.945.9566 RSC# 3702 @www.mil-embedded.com/rsc
Page 1 and 2: OpenSystems Publishing BONUS SHOW D
Page 3 and 4: Discover Condor’s Avionics Embedd
Page 5 and 6: The Critical Path to Transformation
Page 7 and 8: Take a closer look at your encrypti
Page 9 and 10: RSC# @www.mil-embedded.com/rsc
Page 11 and 12: RSC# 11 @www.mil-embedded.com/rsc
Page 13 and 14: Reconfigurable FPGAs Hardware PMC/X
Page 15 and 16: Reconfigurable FPGAs Hardware PCI M
Page 19 and 20: Reconfigurable FPGAs Hardware space
Page 23 and 24: Coordinated Performance with Phoeni
Page 25 and 26: when the contract focus and difficu
Page 27 and 28: Software-Defined Radios (SDRs) Soft
Page 29 and 30: HighRel PC/PCI-104 Modules and Syst
Page 31 and 32: Software-Defined Radios (SDRs) Soft
Page 33 and 34: When failure is not an option. Extr
Page 35: Mil Tech Trends should be active at
Page 39 and 40: PC/104-Plus with Pentium ® M DIGIT
Page 41 and 42: THE FUTURE OF ELECTRONIC SYSTEMS FO
Page 45 and 46: 23-25 October 2006 Marriott Wardman
Page 47 and 48: Sonar UAV (BMP (SMP Mode) QNX Neutr
Page 49 and 50: Product Guide multiprocessors Multi
Page 51 and 52: Product Guide MULTIPROCESSORS Multi
Page 53 and 54: Military EMBEDDED SYSTEMS A N O P E
Page 55 and 56: GE Fanuc Embedded Systems Imagine w

Military Embedded Systems Summer 2006

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?