HH60J:  OPINICUS Corporation accomplished the design and interfacing of the hardware and software for the stimulation of the Digital Autoflight Control System (DAFCS) to model all high speed analog actuators that interface with the DAFCS black box; we were responsible for the design and interface of the stability augmentation system, stabilator system, PBA system, flight/rotor- dynamics (NASA ARMCOMP), Autotest, and motion cues tuning, all through acceptance.  We completed the: interface/modification/test/ acceptance of Fokker MICoL Digital Control Loading System.  We utilized a Motorola RISC based Harris Nighthawk computer system coded in Ada.

CH46:  We completed design, code and test of the flight/rotor-dynamics (Blade Element) automatic flight control system, flight controls and electric control loading interface software in Fortran.

CH53:  We completed design, code and test of the flight/rotor-dynamics, automatic flight control system, flight  control, and electric control loading interface software in Fortran.

MH60G OFT:  We were under contract to integrate and test new engines software on the target computer system.  To develop a follow-on 60G
utilizing a three channel visual system and four channel electric control loading system.  The software was compiled on a SUN workstation and down loaded via ethernet to VME Force 68040 microprocessors.  Areas of design included 701 engines and control loading interface to the electronic control loading system.

MH60G WST:  We were responsible for the automated flight, engines, and control test system software, flight dynamics software, GE Compuscene V interface software, motion/visual/ seat shaker cue correlation, motion, seat shaker tuning, control loading interface, flight controls, autoflight, aircraft systems, navigation systems, radio station database design, VMIC-IO, VOR/ILS/ TACAN/LF-ADF from design through government test.

SH-3:  We are currently under contract and are responsible for the Automatic Fidelity Testing system (AFT) and AFT Trimmers.  In addition, we are supporting our customer in areas of Nav/Com, I/O, Code & Test, Control Loading, and Rotor Dynamics.  As a result of our expertise, our customer has requested a strategic alliance between our companies for specific projects.


3000H Loader
OPINICUS offers a range of High Force, high fidelity loaders to meet the requirements for all aircraft types, and to surpass the overall performance and reliability of hydraulic control loading systems.  The REALFEEL® system replicates the forces required for an adequate simulation of the complete performance envelope, including control jam malfunctions, and high sustained pedal forces required for engine out training scenarios, as well as other emergency procedures.

REALFEEL® digital electric control loading systems have been installed on the following simulators:  CH-53E, CH46E, EA6 OFT, C130H WST, C130E WST, C130 TWST, EA6B, DC9-30,
REALFeelTM 3000H
CN-235, Z11, B737, MV22 DC8, B767, A320, 


EH101, AH1W, etc.

REALFEEL® is selected by LMSTS for the Marine Corps Aviation Simulation Master Plan.
 

OPINICUS Corporation applies Turnkey Solutions and state-of-the-art technologies to every simulator effort.  Our areas of expertise include: REALFeel® electric control loading, new simulators, simulator moves, and simulator upgrades.

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OPINICUS Corporation
1827 NorthPointe Pkwy
Lutz, Florida 33558