ASTOR Flight Manual For Single Crew Members [CA 5.3, April 2014] ♦♦ Double Black Aviation Technology ASTOR Flight Manual, v1 Q All Aspect Aerospace Innovations PAGE 1 OF 7 Single Crew - ASTOR FLIGHT MANUAL ASTOR Flight Manual 2014 - 04 Revision 1 March 2014 AIRCRAFT SIMULATION FOR TRAFFIC OPERATIONS RESEARCH ...................................................................... 3 ASTOR CONTROLS AND INDICATIONS .................................................................................................................................................. 4 MODE CONTROL PANEL (MCP) ............................................................................................................................................................ 6 PRIMARY FLIGHT DISPLAY (PFD) ........................................................................................................................................................ 7 NAVIGATION DISPLAY (ND) ................................................................................................................................................................... 7 ASTOR Flight Manual, v1 PAGE 2 OF 7 Single Crew - ASTOR FLIGHT MANUAL AIRCRAFT SIMULATION FOR TRAFFIC OPERATIONS RESEARCH The ASTOR simulator has been developed in compliance with existing and advanced avionics system specifications to verify research concepts in a realistic onboard environment. ASTOR models current basic aircraft components that include: • Aircraft and engine models, autopilot and auto-throttle systems • Flight Management Computer (FMC), Primary Flight Display (PFD), Navigation Display (ND) • Engine Indication and Crew Alerting System display (EICAS) • Multi-function Control Display Unit (MCDU), Mode Control Panel (MCP) • Electronic Flight Instrumentation System (EFIS), Electronic Flight Bag (EFB) • Cockpit Display of Traffic Information (CDTI) (shown on the EFB) • Configurable Glass Display (CGD), and the Communications Management Unit (CMU). Figure 1: Layout of CA 5.3 ASTOR Displays ASTOR Flight Manual, v1 PAGE 3 OF 7 Single Crew - ASTOR FLIGHT MANUAL ASTOR CONTROLS AND INDICATIONS The CA 5.3 ASTOR is a single-pilot, medium-fidelity human-in-the-loop computer workstation-based aircraft simulation, which supports research of air traffic operations within future airspace environments. ASTOR displays, indications and warnings are modeled after the Boeing 777 cockpit displays with the aerodynamic performance of a Boeing 757. The left side of the CA 5.3 ASTOR (Figure 2) contains the pilot’s main displays which includes the Primary Flight Display, Navigational Display, a CPDLC Control Panel for data link communications, an Electronic Flight Instrumentation System control panel for the primary displays, an aircraft Mode Control Panel, Multi-function Control Display Unit (MCDU), a Simulation Status Panel and a Transponder Control Panel. Figure 2: Left Side of CA 5.3 ASTOR Displays ASTOR Flight Manual, v1 PAGE 4 OF 7 Single Crew - ASTOR FLIGHT MANUAL The right side of the FIAT-4 ASTOR (Figure 3) includes a NASA designed Configurable Glass Display, a Display Select Panel, an Electronic Flight Bag, the Primary Engine Indication and Crew Alerting System display, a radio tuning panel and a speed brakes, throttles, gear and flap control panel. Figure 3: Right Side of CA 5.3 ASTOR Displays The key components for conducting FIM operations are the CGD and EFB auxiliary displays which will be described in the CA 5.3 IM Pilot Guide. The single pilot CA 5.3 ASTOR workstation is actuated using a computer mouse. A mouse and cursor are used to operate all of the controls on both screens of the ASTOR workstation. The ASTOR displays, controls and indications are all modeled to have functionality similar to Boeing aircraft and are designed to allow pilots that have experience on Boeing aircraft to operate the it with minimum training. Alternate select or push button functions on the ASTOR are actuated by using the mouse to click on the icon. Knob selectable values can be adjusted by clicking on the left side of the knob to lower the associated value and clicking on the right side of the knob to increase the value. When a control has numerical values printed on label the associated value can be selected by clicking on the appropriate number. ASTOR Flight Manual, v1 PAGE 5 OF 7 Single Crew - ASTOR FLIGHT MANUAL MODE CONTROL PANEL (MCP) To actuate a button on the MCP simply click on it with the mouse. Experiment pilots will be required to enter the FIM Commanded speed into the MCP. To select an Air Speed click the center of the button to open or close the MCP “Airspeed Window” and choose a speed by clicking on either of the button. Clicking on the right side of the button increases the value in the window and clicking on the left side of the button decreases the value. Decrease Select Increase Decrease Select Increase Figure 4: ASTOR Mode Control Panel (MCP) CAUTION: ASTOR does not have complete VNAV functionality prior to Top Of Descent (in addition to conflicting documentation from the OEM on what that functionality should be). Therefore, flight crews are instructed to use FLCH or Vertical Speed to initiate a descent to a lower cruise altitude prior to the FMS-calculated TOD if directed to do so by ATC. CAUTION: The FMS cruise page should not be used to update the new cruise altitude. CAUTION: The FMS descent page should not be used to update the descent speed to align with the FIM commanded speed. ASTOR Flight Manual, v1 PAGE 6 OF 7 Single Crew - ASTOR FLIGHT MANUAL PRIMARY FLIGHT DISPLAY (PFD) The ASTOR Primary Flight Display (PFD) is key component for conducting FIM operations. The MCP Commanded speed is located in the upper left corner just above the speed tape. The aircraft’s current speed and acceleration cue are key elements for matching the ASTAR deceleration rate. AIRCRAFT Commanded Airspeed Aircraft’s Current Speed Acceleration Cue Airspeed Bug Figure 5: ASTOR Primary Flight Display (PFD) NAVIGATION DISPLAY (ND) The Vertical Deviation Indicator on the Navigation Display is used by pilots operating the ASTOR to ensure the aircraft remains within +/- 400 feet of the vertical path. Ownship Vertical Deviation Indicator Figure 6: ASTOR Navigational Display (ND) ASTOR Flight Manual, v1 PAGE 7 OF 7
© Copyright 2024