Kanardia Nesis III User manual

Nesis III User’s Manual
©Kanardia d.o.o.
April 2022
Release for software version 3.9

Nesis III User’s Manual
Contact Information
Publisher and producer:
Kanardia d.o.o.
Lopata 24a
SI-3000
Slovenia
Tel: [phone]
Email: [e-mail]
A lot of useful and recent information can be also found on the Internet. See
http://www.kanardia.eu for more details.
Copyright
This document is published under the Creative Commons, Attribution-Share-
Alike 3.0 Unported licence. Full license is available on http://creativecommons.
org/licenses/by-sa/3.0/legalcode web page and a bit more human read-
able summary is given on
http://creativecommons.org/licenses/by-sa/3.0/. In short, the license
gives you right to copy, reproduce and modify this document if:
•you cite Kanardia d.o.o. as the author of the original work,
•you distribute the resulting work only under the same or similar license
to this one.
Credits
This document was written using TeX Live (L
A
T
E
X) based document creation
system using Kile running on Linux operating system. Most of the figures were
drawn using Open Office Draw, Inkscape and QCad applications. Photos and
scanned material was processed using Gimp. All document sources are freely
available on request under the licence mentioned above and can be obtained
by email. Please send requests to [e-mail].
3©Kanardia 2018-2022

Nesis III User’s Manual
WEEE Statement
Disposal of Waste Electrical and Electronic Equipment. This
electrical item cannot be disposed of in normal waste. Check
with your local authority for kerbside collection, or recycle
them at a recycling centre.
Third Party Licensing
Nesis software is using the Qt Library published by The Qt Company. The
LGPLv3 license version is used. Please refer to the License section on page
131 for more details.
Revision History
The following table shows the revision history of this document.
Date Description
Sep 2018 Complete manual rework to match software version 3.3
Jan 2019 SW 3.4: GNSS Constellation window added, CTR is shown
filled, UL Power, MWFly engine, Trig radio, Eagle Flarm,
AIR Traffic support, GSA added to standard NMEA output,
parameter editor enhancements, bug fixes.
Mar 2020 SW 3.6: New traffic message, various counters in info, remov-
ing unnamed waypoints, engine only logs, improved Rotax iS
support, CAS support, WiFi GDL90 support, bug fixes.
Oct 2020 SW 3.7: New route planning page, wired GDL90 support,
trim positions on all screens, METAR reports interpretation,
bug fixes.
Apr 2022 Updated to SW 3.9. Approach chart capability, many minor
fixes and improvements.
4©Kanardia 2018-2022

Nesis III User’s Manual CONTENTS
Contents
1 Introduction 11
1.1 Icons Used Trough the Manual . . . . . . . . . . . . . . . . . . 11
1.2 Warnings .............................. 11
1.3 Cautions............................... 12
2 System Overview 14
2.1 Components in the Nesis System . . . . . . . . . . . . . . . . . 14
2.1.1 Required CAN Bus Components . . . . . . . . . . . . . 14
2.1.2 Optional CAN Bus Components or Accessories . . . . . 15
2.1.3 Optional CAN Bus Displays . . . . . . . . . . . . . . . . 17
3 Display Operation 18
3.1 DisplayOverview.......................... 19
3.1.1 TouchScreen ........................ 20
3.2 TurningON/OFF ......................... 21
3.3 Start-up Sequence . . . . . . . . . . . . . . . . . . . . . . . . . 21
3.4 StatusBar.............................. 21
3.4.1 GDL90 Devices . . . . . . . . . . . . . . . . . . . . . . . 24
3.5 Screens ............................... 24
3.6 ClassicScreen............................ 25
3.7 NavigationScreen ......................... 27
3.7.1 Main Elements of the Navigation Screen . . . . . . . . . 27
3.7.2 Moving the Map Around . . . . . . . . . . . . . . . . . 29
3.7.3 Open Flightmap Association and Map Details . . . . . . 29
3.8 WeatherOverlay .......................... 31
3.8.1 Approach Maps . . . . . . . . . . . . . . . . . . . . . . . 31
3.8.2 Map Layers And Details . . . . . . . . . . . . . . . . . . 32
3.8.3 OFMDetails ........................ 33
3.8.4 Airspace Filter . . . . . . . . . . . . . . . . . . . . . . . 34
3.9 EngineScreen............................ 35
3.10ModernScreen ........................... 36
3.10.1 Modern Screen with Moving Map . . . . . . . . . . . . . 38
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Nesis III User’s Manual CONTENTS
3.10.2 Video ............................ 38
3.11ScreenElements .......................... 38
3.11.1 Airspeed Indicator . . . . . . . . . . . . . . . . . . . . . 39
3.11.2 Small Attitude Indicator . . . . . . . . . . . . . . . . . . 41
3.11.3 Altitude Indicator . . . . . . . . . . . . . . . . . . . . . 42
3.11.4 Tachometer (RPM) and Manifold Pressure Indicator . . 42
3.11.5 Gyroplane Engine RPM, Rotor RPM, Manifold and
Prerotation Indicator . . . . . . . . . . . . . . . . . . . . 43
3.11.6 Helicopter Rotor and Engine RPM Indicator . . . . . . 45
3.11.7 Mini Engine Monitor . . . . . . . . . . . . . . . . . . . . 45
3.11.8 Fuel Computer Monitor . . . . . . . . . . . . . . . . . . 46
3.11.9 OAT, Flight Time, Fuel . . . . . . . . . . . . . . . . . . 47
3.11.10 Direction Indicator . . . . . . . . . . . . . . . . . . . . . 47
3.11.11 Special Markings on Engine Parameters . . . . . . . . . 48
4 Flight Time Activities 49
4.1 MainMenu ............................. 49
4.2 QNH................................. 50
4.2.1 QFESetting ........................ 50
4.2.2 Initial QNH Setting . . . . . . . . . . . . . . . . . . . . 51
4.3 RadioStandby ........................... 51
4.4 Selecting a Waypoint . . . . . . . . . . . . . . . . . . . . . . . . 52
4.4.1 Creating a Marker . . . . . . . . . . . . . . . . . . . . . 53
4.4.2 Waypoint Details . . . . . . . . . . . . . . . . . . . . . . 53
4.5 Route ................................ 54
4.5.1 Activating a Route . . . . . . . . . . . . . . . . . . . . . 55
4.5.2 Creating a New Route – Nesis Without Touch Screen . 56
4.5.3 Creating a New Route – Nesis With Touch Screen . . . 58
4.5.4 Importing a Route . . . . . . . . . . . . . . . . . . . . . 60
4.5.5 Deleting a Route . . . . . . . . . . . . . . . . . . . . . . 61
4.5.6 Renaming a Route . . . . . . . . . . . . . . . . . . . . . 61
4.5.7 Editing a Route . . . . . . . . . . . . . . . . . . . . . . 62
4.5.8 Reversing a Route . . . . . . . . . . . . . . . . . . . . . 62
4.5.9 Actions on an Active Route . . . . . . . . . . . . . . . . 62
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Nesis III User’s Manual CONTENTS
4.6 Adjusting Fuel Level . . . . . . . . . . . . . . . . . . . . . . . . 63
4.7 Setting Pitch Correction . . . . . . . . . . . . . . . . . . . . . . 63
5 Flarm and ADS-B Receivers 64
5.1 Directional and Non-Directional Traffic . . . . . . . . . . . . . 65
5.1.1 Flarm Subsystem . . . . . . . . . . . . . . . . . . . . . . 65
5.1.2 ADS-B in Subsystem . . . . . . . . . . . . . . . . . . . . 65
5.2 Traffic on the Moving Map . . . . . . . . . . . . . . . . . . . . 66
5.3 Warning............................... 67
5.4 Settings ............................... 69
5.4.1 Info ............................. 70
5.4.2 General Settings . . . . . . . . . . . . . . . . . . . . . . 71
5.4.3 ADS-B Settings . . . . . . . . . . . . . . . . . . . . . . . 72
5.4.4 Range Settings . . . . . . . . . . . . . . . . . . . . . . . 73
5.5 Errors ................................ 73
5.5.1 ’New traffic’ messages . . . . . . . . . . . . . . . . . . . 74
6 Engines with ECU 75
6.1 RotaxiS............................... 75
6.1.1 Status details . . . . . . . . . . . . . . . . . . . . . . . . 76
6.2 ULPowerEngines.......................... 77
7 Logbook 78
7.1 ShowDetails ............................ 79
7.2 Copy Flight to USB . . . . . . . . . . . . . . . . . . . . . . . . 81
7.2.1 TheKmlFile........................ 81
7.2.2 TheTabFile ........................ 81
7.3 Copy Logbook to USB . . . . . . . . . . . . . . . . . . . . . . . 83
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Nesis III User’s Manual CONTENTS
8 User Options 84
8.0.1 Password .......................... 84
8.1 Logbook............................... 85
8.2 Routes................................ 85
8.3 Settings ............................... 85
8.3.1 User............................. 86
8.3.2 Units ............................ 88
8.3.3 Range&Fuel........................ 89
8.3.4 Screen............................ 90
8.3.5 Map............................. 91
8.3.6 Logger............................ 92
8.3.7 Maintenance ........................ 93
8.3.8 Engine Shut Down . . . . . . . . . . . . . . . . . . . . . 94
8.3.9 Glide ............................ 95
8.4 Pilots ................................ 96
8.5 Alarms................................ 97
8.5.1 Editing an Alarm . . . . . . . . . . . . . . . . . . . . . . 98
8.6 Brightness.............................. 99
8.7 Audio ................................ 99
8.8 Compass...............................100
8.9 ADSB/Flarm ............................100
8.10Waypoints..............................100
8.10.1 New Waypoint . . . . . . . . . . . . . . . . . . . . . . . 100
8.10.2 Import............................101
8.10.3 Transfer...........................102
8.10.4 Deleteall ..........................102
8.10.5 Delete unnamed . . . . . . . . . . . . . . . . . . . . . . 102
8.10.6 Waypoint Edit/Delete . . . . . . . . . . . . . . . . . . . 102
8.11Maps.................................102
8.11.1 When Copy Fails . . . . . . . . . . . . . . . . . . . . . . 104
8.12Update ...............................104
8.13Wireless...............................105
8.14Info .................................105
8.15Service................................107
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Nesis III User’s Manual CONTENTS
9 Service Options 108
9.1 Password ..............................108
9.2 Icons.................................108
10 Software Update 110
10.1Versioning..............................110
10.2Downgrading ............................110
10.3 Updating with USB Stick . . . . . . . . . . . . . . . . . . . . . 110
10.3.1 Downloading Updates . . . . . . . . . . . . . . . . . . . 111
10.3.2 Copying Update File to the USB Stick . . . . . . . . . . 113
10.3.3 Performing the Update . . . . . . . . . . . . . . . . . . 113
10.4 Direct Update Mode (Emergency Mode) . . . . . . . . . . . . . 114
11 Database Update 114
11.1 Updating with USB Stick . . . . . . . . . . . . . . . . . . . . . 115
11.1.1 Downloading Updates . . . . . . . . . . . . . . . . . . . 115
11.1.2 Copying Update File to the USB Stick . . . . . . . . . . 115
11.1.3 Performing the Update . . . . . . . . . . . . . . . . . . 116
11.2UpdatewithWiFi .........................116
12 Autopilot 116
12.1IntendedUse ............................117
12.2 Operation Limitations . . . . . . . . . . . . . . . . . . . . . . . 117
12.3 System Description . . . . . . . . . . . . . . . . . . . . . . . . . 117
12.4 Autopilot Status Window . . . . . . . . . . . . . . . . . . . . . 118
12.5AutopilotSetup...........................119
12.6 Setting User Button . . . . . . . . . . . . . . . . . . . . . . . . 119
12.7Safety ................................119
12.8Operation..............................119
12.8.1 Track ............................120
12.8.2 Altitude...........................121
12.8.3 Flight Director (HNAV) . . . . . . . . . . . . . . . . . . 121
12.8.4 Disable ...........................122
12.8.5 Level.............................122
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Nesis III User’s Manual CONTENTS
13 Maps 122
13.1Layers ................................122
13.2VectorMaps ............................124
13.2.1 Installing a Vector Map . . . . . . . . . . . . . . . . . . 125
13.3RasterMaps ............................126
13.3.1 DFS.............................126
13.3.2 US Sectionals . . . . . . . . . . . . . . . . . . . . . . . . 127
13.3.3 France – CartaBossy . . . . . . . . . . . . . . . . . . . . 128
13.3.4 UserCharts.........................129
13.3.5 Installing a Raster Map . . . . . . . . . . . . . . . . . . 129
13.4 Installing Approach Maps . . . . . . . . . . . . . . . . . . . . . 130
14 Third Party Software 130
14.1TheQtLibrary...........................131
14.1.1 Modules and Linking . . . . . . . . . . . . . . . . . . . . 131
14.1.2 Source Code and Toolchain . . . . . . . . . . . . . . . . 131
14.1.3 Compiling The Library . . . . . . . . . . . . . . . . . . 131
14.1.4 Installing Modified Qt Library . . . . . . . . . . . . . . 132
14.1.5 Copy of Qt License Document . . . . . . . . . . . . . . 133
15 Limited Conditions 134
15.1Warranty ..............................134
15.2TSOInformation..........................136
10 ©Kanardia 2018-2022

Nesis III User’s Manual 1. Introduction
1 Introduction
First of all we would like to thank you for purchasing our product. Nesis is a
complex instrument and we strongly recommend reading the manual before
using Nesis. The introduction chapter contains some general information
about the instrument and principles of the operation. Later chapters describe
Nesis use and reveal the details. You may be also interested in reading:
•Nesis Installation Manual,
•DAQU Installation Manual,
•MAGU Manual,
•our web page www.kanardia.eu.
1.1 Icons Used Trough the Manual
A few icons appear on the side of the manual, which have special meanings:
This icon denotes information that needs to be taken with special
attention.
This icon denotes background information about the subject.
This icon denotes a tip.
This icon denotes a touchscreen action.
1.2 Warnings
The following warnings and limitations apply, when you use this instrument.
Failing to do so, may result in significant injuries or even death.
•Before using the instrument, you shall carefully review and understand
the Nesis system and Operating Handbook of the aircraft.
•Information from the Aircraft Operating Handbook always supersedes
Nesis information.
•Use of any navigational data contained by Nesis is entirely at the pilot’s
risk.
11 ©Kanardia 2018-2022

Nesis III User’s Manual 1.3 Cautions
•Carefully compare Nesis navigational information with other available
navigational sources. In the case of any discrepancies, resolve them
before proceeding with the navigation.
•The navigational data used in Nesis comes from various public domain
and open data sources. Although the data was carefully crosschecked
(where this was possible), the data may contain serious errors. The pilot
is obliged to verify any navigational information provided by Nesis, with
the relevant official sources, AIPs, Notams, etc.
•Databases in Nesis must be updated regularly in order to stay current.
Such databases are freely available from our web site.
•Terrain elevation data shall not be used for terrain separation. Its use
is informative only. The pilot must always fly in VFR conditions and
he must maintain visual separation.
•Do not rely on the traffic information and traffic warnings. It is solely
the pilot responsibility to look out, to see and avoid other aircraft. The
other aircraft position depicted on the screen may be wrong due to lack
of proper equipment, poor reception and inaccurate or old information.
•Do not use weather information for maneuvering in, near, or around
areas of hazardous weather. Weather information may not accurately
depict current weather conditions.
•Never use Nesis to attempt to penetrate a thunderstorm. Always avoid
any thunderstorm at least 30 km.
•The Global Positioning System is operated by the United States gov-
ernment, which solely responsible for its accuracy and maintenance. In
a similar way, Russian government is responsible for the GLONASS
system. The GNSS systems are subject to changes which could affect
the accuracy and performance of all GNSS equipment. Therefore, the
navigation information can be misused or misinterpreted and become
unsafe.
1.3 Cautions
•The Nesis display uses special coating, which is sensitive to abrasive
cleaners or cleaners which are using strong chemicals like ammonia or
alike. Always use a lint-free soft cloth and mild cleaning solution or just
pure water.
12 ©Kanardia 2018-2022

Nesis III User’s Manual 1.3 Cautions
•Nesis does not have any serviceable parts. Repairs must be done only by
authorized service centers. An unauthorized repair could void warranty.
•Due to high complexity of the system, the pilot must accept that pro-
viding self-test capability for all possible system failures is not practical.
This means that an erroneous operation may occur without a fault in-
dication or warning. This makes the pilot responsible to detect such an
occurrence by means of cross-checking with all redundant or correlated
information available.
13 ©Kanardia 2018-2022

Nesis III User’s Manual 2. System Overview
2 System Overview
2.1 Components in the Nesis System
The Nesis System consists of several electronic components, which work closely
together to bring flight, engine and fuel information onto graphical display.
The system consists of various components, some of these are required and
some are optional.
2.1.1 Required CAN Bus Components
Majority of these components communicate trough CAN bus. This section
list components and explains their interaction. Please note that photos are
not in scale.
Nesis master display is the major part of the sys-
tem. It acts as a primary multi-functional dis-
play. Internally it hosts an embedded computer and
an AD-AHRS-GPS module called AIRU. The em-
bedded computer reads information from the CAN
bus and translates it into graphics you see on the
screen. The AIRU module consists of multiple sen-
sors: absolute pressure sensor for altitude and ver-
tical speed, differential pressure sensor for airspeed,
3 axis angular rate and 3 axis accelerometer sensors
for artificial horizon, GPS sensor for position and
OAT probe for true airspeed. Sensor readings are
passed trough various mathematical models which
in turn put the information on the CAN bus. AIRU
is actually an independent device mounted inside
Nesis for convenience.
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Nesis III User’s Manual 2.1 Components in the Nesis System
Engine monitoring (called DAQU) is required to
read the engine, fuel and aircraft related sensors
and to put the obtained information on the CAN
bus. It has three digital channels (Z1, Y1 and Y2),
twenty analog channels (A, B, C, D) and a spe-
cial manifold pressure connector (A13). DAQU also
hosts +5/+12 V power output and ground (GND).
Digital channels are typically used to read engine
or rotor RPM and fuel flow sensors. Analog chan-
nels are typically used to measure CHTs, EGTs,
coolant temperature, oil temperature, carburetor
temperature, airbox/gearbox temperature, fuel lev-
els, system voltage, electrical current, oil pressure,
fuel pressure, hydraulics pressure, pitch trim, flap
position and many others.
DAQU comes in three forms:
•Standard Daqu is typically used with carbu-
retted engines like Rotax 912 UL, ULS, Rotax
914, Jabiru, Lycoming, Continental, etc.
•Mini DAQU is typically used with an engine
that has its own ECU. Rotax iS, D-motor,
Geiger Wankel, MW, etc.
•In some cases there is not enough channels
on mini DAQU. In this case, standard DAQU
modified for ECU engine can be also used.
2.1.2 Optional CAN Bus Components or Accessories
Components listed below are all optional. This means they are not required
for normal Nesis operation.
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Nesis III User’s Manual 2.1 Components in the Nesis System
Electronic Compass (called MAGU) is a stand alone
unit which measures magnetic field vector. It serves
as a gyro stabilized compass and provides true and
magnetic heading with high accuracy. It features
an intelligent calibration algorithm, where only one
known magnetic direction is needed to calibrate it.
MAGU provides heading information on the CAN
bus. With this information available, wind direc-
tion and wind speed is also derived by AIRU unit.
Tail install and nose install versions of MAGU exist.
When two servo units (called SERU) are added to
the CAN bus, the system also performs the autopi-
lot function. Two different SERU units are avail-
able. Stronger and heavier has 6 Nm (53 in lb)
torque, while the lighter and weaker has 3 Nm (27
in lb) torque.
Remote autopilot panel (called AMIGO) brings fur-
ther enhancements to the autopilot functionality.
It allows very simple and straightforward autopilot
operation.
One or two remote control handles (called JOYU)
can be added to the system. The handle allows al-
most complete control of the Nesis display with the
buttons on the top. Buttons are fully configurable
by Nesis. When BOXI unit is also present, it can
also drive roll and pitch trim, radio transmission
button (push-to-talk).
Trim and radio controller called (BOXI) must be
used together with a JOYU handle. You can con-
nect two trim motors to BOXI and then use JOYU
handle to drive them. In addition, radio push-to-
talk wiring can be made directly to BOXI.
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Nesis III User’s Manual 2.1 Components in the Nesis System
Dimu is a dimming device. Its only job is to adjust
LCD brightness of all devices connected to the CAN
bus with a simple rotation of the knob. It also
provides analogue output for third-party devices.
Small WiFi plug is used to connect Nesis to the
WiFi network. This can be done with the help of
a network access point created on a mobile phone
and Nesis is connected to the Internet as long as
the mobile phone is also connected. Alternatively,
some public WiFi hot-spot can be also used, while
aircraft is on the ground. Such connection can be
used to make software updates, map and airspace
updates and to access weather information.
An external carbon monoxide (CO) sensor can be
connected directly to Nesis. In the case of elevated
CO concentration buildup, a visual and acoustic
alarm will appear.
2.1.3 Optional CAN Bus Displays
The system can be extended with several displays. All these displays are
optional. They have no internal sensors. They get the information from the
CAN bus.
Slave Nesis Display can be added to the system. It
has the same functionality as the master Nesis. The
only difference is that it does not host the AIRU
unit and that some system tuning options are not
accessible.
Slave AETOS display with diagonal size 7 inches is
very similar to slave NESIS display. The AETOS
display does not have touch screen and there are
no maps available, however it includes 3D synthetic
vision.
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Nesis III User’s Manual 3. Display Operation
A small slave display (called EMSIS) comes in two
forms. The first fits into 80 mm standard aviation
opening, the second is larger with 3.5 inch diagonal
and has more complex shape. They both can be
viewed as small EFIS displays. EMSIS can show
basic primary flight and engine monitor values.
A rectangular, very slim and very light LCD display
(called DIGI) is typically used to show engine val-
ues. The values can be shown in the form of arcs,
bars, boxes and values. Start of display is very fast.
You can read oil pressure almost immediately, while
Nesis primary display is still booting.
One or more slave round instruments can be added
to the bus. They can show almost any value, which
is available on the bus. The most typical are: air-
speed indicator, altimeter, vertical speed indicator,
engine RPM, rotor RPM, G-meter, etc. All indica-
tors consists of a needle pointing to a scale and a
LCD display. Pointer is driven by a stepper motor.
Needle shows one value, but LCD display may show
up to three different parameters.
HORIS slave primary flight display can comple-
ment the Nesis system, too. HORIS can show PDF
screen, DI screen or G-meter screen.
3 Display Operation
This section will familiarize you with basic procedures referring to PFD, EMS
and moving map operations.
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Nesis III User’s Manual 3.1 Display Overview
3.1 Display Overview
The Nesis command panel is organized according to Figure 1. It uses three
push buttons and one push knob for manipulation. It has an USB port for
software, map and data updates. Most of the actions can be also done using
the touch screen.
23456
1
Figure 1: Organization of the Nesis display.
Here is a brief description of individual items:
1
○The touch screen. It works just as touch on tablets and telephones do.
It detects single touch, long single touch, multi touch, touch and drag,
swipe.
2
○The Selector knob detects knob rotation, short push and long push. It
is mostly used to select things, confirm selection, change values, change
zoom levels, etc. Rotate the knob to select things and push the knob to
confirm. Long push action opens the options screen.
3
○A short push on the button will perform Close/Back/Cancel commands.
It is mostly used to close opened windows, to go back or to cancel some
action. Long push action is user configurable.
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Nesis III User’s Manual 3.1 Display Overview
4
○The User button. Both, short and long push are user configurable.
By default it shows the list of nearest airports and when autopilot is
detected, it starts the autopilot actions.
5
○A short push on the Screen-switching button is used to switch to the
next screen. Long push action is user configurable.
6
○The USB port is used for software, map and data updates, to copy the
flights and logbook, etc.
In most cases you only use the selector knob and the close button.
Short push is defined as a momentarily press and release of the button. An
associated action is activated on the release.
Long push is defined as a press-and-hold of the button. Button must be
pressed and keep pressed for about two seconds. An associated action will
be activated after two second period even if the button was not released yet.
Nothing happens on release.
3.1.1 Touch Screen
The touch screen significantly simplifies handling and proves to be very help-
ful. It behaves in a similar way as most smart telephones and tablets do.
Additionally it supports some swipes (gestures) listed below:
•A swipe across the screen to the left switches to the next screen;
•A swipe across the screen to the right switches to the previous screen;
•A swipe upwards opens the main menu;
•A touch on the navigation point on the main navigation screen activates
this point in the direct-to mode. When more points are in the vicinity,
a list of points is displayed;
•A touch on the round altimeter opens the QNH window;
•A touch on the classic screen map opens the navigation screen;
More touch actions are revealed throughout the manual.
20 ©Kanardia 2018-2022