### © 201 5 DJI . All Rights Reserved. 

# N aza - M V2

Quick Start Guide V 1 .2 8

201 5 .0 6 .1 2 Revision

For Firmware Version V 4.0 4 or above

& Assistant Software 

## Version V2. 40 or above

Thank you for purchasing this DJI product. Please strictly follow thes e steps to mount and connect th is system on

your aircraft, as well as to install the Assistant Software on your computer.

Please regularly check the web page of corresponding product 

# * at our website 

# www.dji.com , which is

updated regularly. Product information, technical updates and manual correctio ns will be available on this web

page. Due to unforeseen changes or product upgrades, the information contained in this manual is subject to

change without notice.



# * Important: Naza

- M, Naza

- M V2 and PHANTOM control system are different in hardware part s, but their
configurations and functions are the same when using the same Assistant Software and Firmware Version, so they

use the same Guide. Unless stated, the following instruction is basic on Naza

- M V2. If you use the Naza

- M, please

make sure to read the “ Instruction of V1 (also known as Naza

- M) ” section ; if you use the PHANTOM, download the

other corresponding manual s on the PHANTOM web page

.

This manual is only for basic assembly and configuration; you can obtain more details and advanced instructions

when using the assistant software. To assure you have the latest information, please visit our website and download

the latest manual and current software version.

If you have any problem that you cannot solve during usage, please contact your authorized dealer.

### © 201 5 DJI . All Rights Reserved. 

# Index

INDEX

................................ ................................ ................................ ................................ ................................ ............... 2

INSTRUCTION

................................ ................................ ................................ ................................ ................................ . 3

D ISCLAIMER 

## & W ARNING



## ................................ ................................ ................................ ................................ .................... 3
T RADEMARK



## ................................ ................................ ................................ ................................ ................................ ..... 4
C ERTIFICATIONS



## ................................ ................................ ................................ ................................ ................................ . 4
S YMBOL 

## I NSTRUCTION



## ................................ ................................ ................................ ................................ ......................... 4

ASSEMBLY & CONNECTIO N

................................ ................................ ................................ ................................ ........ 5

S TEP 

## 1 P ORT 

## D ESCRIPTION



## ................................ ................................ ................................ ................................ ................... 5
S TEP 

## 2 A SSEMBLY 

## & C ONNECTION



## ................................ ................................ ................................ ................................ ......... 6

ASSISTANT SOFTWARE I NSTALLATION AND CONF IGURATION

................................ ................................ ............ 7

S TEP 

## 1 S OFTWARE AND 

## D RIVER 

## I NSTALLATION



## ................................ ................................ ................................ .......................... 7
S TEP 

## 2 C ONFIGURATION BY 

## A SSISTANT ON A 

## PC

................................ ................................ ................................ ........................ 8

BASIC FLYING

................................ ................................ ................................ ................................ ............................... 10

C ONTROL 

## M ODE 

## K NOWLEDGE



## ................................ ................................ ................................ ................................ ............ 10
S TART 

## & S TOP 

## M OTOR 

## K NOWLEDGE



## ................................ ................................ ................................ ................................ .... 10
S TEP 

## 1 C OMPASS 

## C ALIBRATION



## ................................ ................................ ................................ ................................ ............ 12
S TEP 

## 2 A SSEMBLY 

## C HECKING 

## L IST



## ................................ ................................ ................................ ................................ ......... 13
S TEP 

## 3 B EFORE 

## F LIGHT



## ................................ ................................ ................................ ................................ ...................... 13
S TEP 

## 4 F LYING 

## T EST



## ................................ ................................ ................................ ................................ ........................... 14

ADVANCED FUN CTIONS

................................ ................................ ................................ ................................ ............ 16

A1 F AIL 

## S AFE



## ................................ ................................ ................................ ................................ ................................ ... 16
A2 L OW



## - V OLTAGE 

## A LERT



## ................................ ................................ ................................ ................................ ................... 17
A3 I NTELLIGENT 

## O RIENTATION 

## C ONTROL 

## (IOC) F LIGHT 

## ( WITH 

## GPS MODULE 

## )

................................ ................................ ............... 18
A4 R ECEIVER 

## A DVANCED 

## P ROTECTION 

## F UNCTION



## ................................ ................................ ................................ ................... 21
A5 F LIGHT 

## L IMITS



## ................................ ................................ ................................ ................................ ............................ 22

APPENDIX

................................ ................................ ................................ ................................ ................................ ..... 23

S PECIFICATIONS



## ................................ ................................ ................................ ................................ ............................... 23 MC/PMU F IRMWARE 

## U PGRADE



## ................................ ................................ ................................ ................................ ........ 24
LED D ESCRIPTION



## ................................ ................................ ................................ ................................ ............................ 25

INSTRUCTION OF V1 ( ALSO KNOWN AS NAZA

- M)

................................ ................................ ................................ .. 26

V1 A SSEMBLY AND 

## C O NNECTION



## ................................ ................................ ................................ ................................ ......... 26
V1 IS COMPATIBLE WITH T HE 

## PMU V2 (A CCESSORY OF 

## N AZA



## - M V2)

................................ ................................ ......................... 26
V1 P ORT 

## D ESCRIPTION



## ................................ ................................ ................................ ................................ ...................... 27
V1 S PECIFICATION



## ................................ ................................ ................................ ................................ ............................ 28

FAQ

................................ ................................ ................................ ................................ ................................ ................ 29

A BNORMAL 

## LED I NDICATION 

## L IST



## ................................ ................................ ................................ ................................ ........ 29
F IX THE 

## TBE (T OILET 

## B OWL 

## E FFECT 

## ) P ROBLEM



## ................................ ................................ ................................ ....................... 29
S HOULD YOU FIND THE M ULTI



## - ROTOR DOES NOT TRACK STRAIGHT IN FORWARD FLIGHT



## . ................................ ................................ ... 30
M OTORS 

## S TART FAILURE CAUSED BY 

## TX STICK 

## ( S 

## ) MID



## - POINT ERROR TOO BIG



## ................................ ................................ ................. 30
A

TTITUDE 

## C ONTROLLABLE 

## W HEN 

## O NE 

## M OTOR 

## O UTPUT IS 

## F AILED



## ................................ ................................ .............................. 31
W HEN USED WITH OTHER 

## DJI PRODUCTS



## ................................ ................................ ................................ .............................. 31

### © 201 5 DJI . All Rights Reserved. 

## 3 | 

# Instruction Disclaimer & Warning Please read this disclaimer carefully before using the product. By using this product, you hereby agree to this disclaimer and signify that you have read them fully. THIS PRODUCT IS NOT
SUITABLE FOR PEOPLE UNDER THE AGE OF 18.

This product is an autopilot system designed for serious multi

- rotor enthusiasts providing excellent self

- leveling and
altitude holding, which completely takes th e stress out of flying RC multi

- rotors for both professional and hobby
applications. Despite the system having a built

- in autopilot system and our efforts in making the operation of the
controller as safe as possible when the main power battery is connecte d, we strongly recommend users to remove
all propellers when calibrating and setting parameters. Make sure all connections are good, and keep children and
animals away during firmware upgrade, system calibration and parameter setup. DJI Innovations accepts no liability for damage(s) or injuries incurred directly or indirectly from the use of this product in the following conditions:

1. Damage(s) or injuries incurred when users are drunk, taking drugs, drug anesthesia, dizziness, fatigue, nausea

and any other c onditions no matter physically or mentally that could impair your ability.

2. Damage(s) or injuries caused by subjective intentional operations. Any mental damage compensation caused

by accident.

3. Failure to follow the guidance of the manual to assemble or ope rate.

4. Malfunctions caused by refit or replacement with non

- DJI accessories and parts.

5. Damage(s) or injuries caused by using third party products or fake DJI products.

6. Damage(s) or injuries caused by mis

- operation or subjective mis

- judgment.

7. Damage(s) or in juries caused by mechanical failures due to erosion, aging.

8. Damage(s) or injuries caused by continued flying after low voltage protection alarm is triggered.

9. Damage(s) or injuries caused by knowingly flying the aircraft in abnormal condition (such as water , oil, soil,
sand and other unknown material ingress into the aircraft or the assembly is not completed, the main
components have obvious faults, obvious defect or missing accessories).

10. Damage(s) or injuries caused by flying in the following situations suc h as the aircraft in magnetic interference
area, radio interference area, government regulated no

- fly zones or the pilot is in backlight, blocked, fuzzy
sight, and poor eyesight is not suitable for operating and other conditions not suitable for operating.

11. Damage(s) or injuries caused by using in bad weather, such as a rainy day or windy (more than moderate
breeze), snow, hail, lightning, tornadoes, hurricanes etc.

12. Damage(s) or injuries caused when the aircraft is in the following situations: collision, fir e, explosion, floods,
tsunamis, subsidence, ice trapped, avalanche, debris flow, landslide, earthquake, etc.

13. Damage(s) or injuries caused by infringement such as any data, audio or video material recorded by the use of

aircraft.

14. Damage(s) or injuries cause d by the misuse of the battery, protection circuit, RC model and battery chargers.

15. Other losses that are not covered by the scope of DJI Innovations liability.

### © 201 5 DJI . All Rights Reserved. 

## 4 | 

# Trademark

DJI and N aza

- M are registered trademarks of DJI Innovations. Names of product, brand, etc., appearing in this

manual are trademarks or registered trademarks of their respective owner companies. This product and manual are

copyrighted by DJI Innovations with all rights reserved. No part of this product or manual shall be reproduced in

any f orm without the prior written consent or authorization of DJI Innovations. No patent liability is assumed with

respect to the use of the product or information contained herein.



# C ertifications

This product is approved with quality standards such as CE, FC C and RoHS.



# Symbol Instruction

Forbidden(Important) Cautions Tip Reference

### © 201 5 DJI . All Rights Reserved. 

## 5 | 

# Assembly & Connection

In the Box:

Main controller X1, PMU X1, GPS X1, GPS Bracket X1, LED X1, Servo Cable X 8

, Micro

- USB Cable X1, 3M A dhesive

T ape

. 

# Step1 Port Description

L E D : C o n n e c t t o L E D m o d u l e E X P : C o n n e c t t o P M U m o d u l e

M 1 : T o # 1 E S C ( * ) M 2 : T o # 2 E S C M 3 : T o # 3 E S C M 4 : T o # 4 E S C M 5 : T o # 5 E S C M 6 : T o # 6 E S C F 1 : T o g i m b a l r o l l s e r v o o r T o # 7 E S C F 2 : T o g i m b a l p i t c h s e r v o o r T o # 8 E S C N A Z A o u t p u t i s 4 0 0 H z r e f r e s h f r e q u e n c y A : F o r r o l l c o n t r o l ( l e f t / r i g h t ) E : F o r p i t c h c o n t r o l ( f r o n t / b a c k ) T : F o r t h r o t t l e c o n t r o l R : F o r r u d d e r c o n t r o l U : F o r C o n t r o l M o d e l S w i t c h X 1 : F o r g i m b a l p i t c h c o n t r o l / F o r g a i n t u n i n g X 2 : F o r D

- B u s ( S

- B u s / S

- B u s 2 c o m p a t i b l e ) / F o r g a i n t u n i n g / F o r I O C s w i t c h X 3 : F o r v o l t a g e m o n i t o r ( C o n n e c t t o P M U V

- S E N p o r t )

G P S : C o n n e c t t o G P S / C o m p a s s m o d u l e

E x t e n d e d C A N p o r t 2 S ~ 6 S : P o w e r e d b y 2 S ~ 6 S L i P o ( 7

. 4 V ~ 2 6

. 0 V )

E X P : C o n n e c t t o M a i n C o n t r o l l e r E X P p o r t

C o n n e c t t o M a i n C o n t r o l l e r L E D p o r t

M i c r o

- U S B : P C c o n n e c t i o n f o r p a r a m e t e r c o n f i g u r a t i o n
a n d f i r m w a r e u p g r a d e

C o n n e c t t o G P S p o r t o f P M U P o i n t i n g t o t h e a i r c r a f t n o s e d i r e c t i o n



## M a i n C o n t r o l l e r

M a i n C o n t r o l l e r P M U ( P o w e r M a n a g e m e n t U n i t )



## L E D

G P S /

C o m p a s s P o i n t i n g t o t h e a i r c r a f t n o s e d i r e c t i o n



### * E S C : E l e c t r o n i c S p e e d C o n t r o l l e r V

- S E N : C o n n e c t t o M a i n C o n t r o l l e r X 3 P o r t I m p o r t a n t : t h e c o n t i n u o u s o u t p u t o f t h e P M U i s 3 A @ 5 V

, a n d t h e m a x i m u m i n s t a n t c u r r e n t i s 7

. 5 A

. I f P M U c a n n o t a f f o r d t h e w o r k i n g c u r r e n t f o r y o u r s e r v o s , p l e a s e

u s e a n i n d e p e n d e n t p o w e r s u p p l y ; o t h e r w i s e , i t m a y c a u s e t h e P M U s a f e g u a r d a n d l e a d t o t h e m a i n c o n t r o l l e r r e b o o t
。

### © 201 5 DJI . All Rights Reserved. 

## 6 | 

# Step 2 Assembly & Connection

T r a n s m i t t e r ( T X ) & R e c e i v e r ( R X ) ( 1 ) R e f e r t o y o u T X M a n u a l

, s e t u p t h e A i l e r o n , E l e v a t o r , T h r o t t l e , R u d d e r
c h a n n e l s o n y o u r T X f i r s t

, a n d c h o o s e a 3

- p o s i t i o n s w i t c h a s c o n t r o l m o d e s w i t c h

. ( 2 ) A t t a c h t h e m a t c h e d R X t o a i r c r a f t

, t h e n
c o n n e c t y o u r R X t o t h e r i g h t p o r t s o n M C

. T h e f o l l o w i n g d i a g r a m s h o w s t h e
c o n n e c t i o n e x a m p l e f o r t r a d i t i o n a l R X

. 

### E S C s E S C s & M o t o r s P l e a s e u s e t h e E S C s a n d m o t o r s r e c o m m e n d e d b y t h e m a n u f a c t u r e r
o f y o u r a i r c r a f t

. W e r e c o m m e n d y o u u s e D J I m o t o r s a n d E S C s ( R e f e r t o i t s m a n u a l f o r d e t a i l s )

. C o n n e c t a l l E S C s t o M C b y t h e m o t o r

n u m b e r i n g m e t h o d i n t r o d u c e d i n m i x e d t y p e s S u p p o r t e d

. I m p o r t a n t : I f y o u u s e 3 r d p a r t y E S C s , m a k e s u r e t h e E S C s t r a v e l

m i d p o i n t i s a t 1 5 2 0 u s

. D O N O T u s e 7 0 0 u s t r a v e l m i d p o i n t E S C

, a s i t

m a y l e a d a i r c r a f t t o f l y a w a y o r c a u s e i n j u r y a n d d a m a g e

. A f t e r E S C s
c o n n e c t i o n , c a l i b r a t e E S C s o n e b y o n e t h r o u g h t h e r e c e i v e r d i r e c t l y b e f o r e c o n n e c t t h e m t o y o u r M C

, M a k e s u r e p r o g r a m a l l o f t h e m i n t o G o v e r n o r o f f

, B r e a k o f f a n d N o r m a l S t a r t u p t o g e t b e s t e x p e r i e n c e

. Q u a d

- r o t o r X H e x a - r o t o r I H e x a - r o t o r V

H e x a - r o t o r Y I m p o r t a n t : T o c o a x i a l p r o p e l l e r s : B l u e p r o p e l l e r i s a t T O P ; R e d p r o p e l l e r i s a t B o t t o m

. O t h e r w i s e a l l p r o p e l l e r s a r e a t t o p

.

Q u a d

- r o t o r I H e x a - r o t o r I Y

F 1 F 2

R o l l P i t c h 

### M a i n C o n t r o l l e r ( M C ) M o u n t : ( 1 ) T h e D J I l o g o s h o u l d f a c e t h e s k y , D O N O T m o u n t t h e M C u p s i d e

- d o w n

. ( 2 ) T h e M C s i d e s
s h o u l d b e p a r a l l e l t o t h e a i r c r a f t b o d y

. ( 3 ) T h e a r r o w
s h o u l d p o i n t t o t h e n o s e d i r e c t i o n o f a i r c r a f t

. ( 4 ) h e M C i s b e s t p o s i t i o n e d n e a r t h e a i r c r a f t ’ s c e n t e r o f g r a v i t y

. M a k e s u r e a l l p o r t s a r e a c c e s s i b l e

. T i p : I t i s r e c o m m e n d e d t o f i x t h e M C u n t i l a l l

w i r i n g s a n d c o n f i g u r a t i o n s a r e c o m p l e t e d

, u s i n g 3 M g u m m e d p a p e r p r o v i d e d t o f i x t h e M C

.



### ( O p t i o n a l ) G P S / C o m p a s s M o u n t : G P S / C o m p a s s i s s e n s i t i v e t o

m a g n e t i c i n t e r f e r e n c e , s h o u l d b e f a r
a w a y f r o m a n y e l e c t r o n i c d e v i c e s

. I f y o u u s e y o u r o w n m o u n t i n g r o d

, m a k e s u r e i t i s N O T m a g n e t i c ! P r o c e d u r e s : ( 1 ) Y o u s h o u l d u s e e p o x y r e s i n A B g l u e t o a s s e m b l e t h e G P S b r a c k e t f i r s t

. M o u n t t h e b r a c k e t o n t h e c e n t e r p l a t e o f c r a f t

. P o s i t i o n t h e b r a c k e t a t l e a s t 1 0 c m f r o m a n y p r o p e l l e r

. ( 2 ) T h e D J I l o g o m a r k e d o n t h e G P S

s h o u l d f a c e t h e s k y , w i t h t h e
o r i e n t a t i o n a r r o w p o i n t i n g d i r e c t l y f o r

w a r d

. t h e n f i x t h e G P S o n t h e p l a t e
o f t h e b r a c k e t ( b y 3 M g l u e p r o v i d e d )

. T i p : T h e G P S / C o m p a s s i s p a c k a g e d

w i t h a s p e c i a l i n d i c a t i o n l i n e f o r

m o u n t i n g f o r t h e f i r s t t i m e

. 

### G i m b a l C o n n e c t t h e g i m b a l s e r v o s t o t h e p o r t s o f F 1 a n d F 2 i f a g i m b a l i s u s e d

, a n d u s e t h e
s o f t w a r e f o r c o n f i g u r a t i o n s

.



### P M U M o d u l e M o u n t : D O N O T a t t a c h t h e P M U o n
o t h e r d e v i c e

. S u f f i c i e n t a i r f l o w o v e r t h e P M U i s h i g h l y r e c o m m e n d e d

. T i p : I f u s e w i t h D J I m u l t i

- r o t o r , y o u
c a n s o l d e r t h e p o w e r c a b l e t o p o w e r p a d s o n f r a m e b o t t o m b o a r d

. P l e a s e

r e f e r t o D J I m u l t i

- r o t o r m a n u a l f o r d e t a i l s

. I f u s e w i t h 3 r d p a r t a i r c r a f t

, y o u c a n m a k e a c o n n e c t e r b y y o u r s e l f t o c o n n e c t P M U a n d b a t t e r y

.


### L E D M o d u l e M o u n t : M a k e s u r e Y o u c a n s e e t h e l i g h t d u r i n g t h e f l i g h t

. L e a v e t h e U S B i n t e r f a c e t o b e a c c e s s i b l e

. U s e t h e 3 M g u m m e d p a p e r p r o v i d e d t o f i x

. E S C & M C C o n n e c t i o n

( J R ) R U D D T H R O A I L E E L E V

3

- p o s i t i o n S w i t c h

( F u t a b a / H i t e c ) 4 3 1 2 

### S t e p 1 P r e p a r e a n a i r c r a f t

, s u p p o r t e d t h e f o l l o w i n g M i x e d T y p e s

.

A i r c r a f t M 1 M 2 M 3 M 4 M 5 M 6 M 7 M 8 M a i n C o n t r o l l e r M 1 M 2 M 3 M 4 M 5 M 6 F 1 F 2 T h e d i r e c t i o n o f t h e a r r o w i n d i a g r a m i n d i c a t e s t h e r o t a t i o n d i r e c t i o n o f t h e m o t o r / p r o p e l l e r

.

O c t o - r o t o r I O c t o - r o t o r V O c t o - r o t o r X

3

- p o s i t i o n S w i t c h 

### S t e p 2 A s s e m b l y a n d C o n n e c t i o n

S t e p 3 D o u b l e C h e c k

I n t h i s s t e p , t u r n o n t h e t r a n s m i t t e r , c o n n e c t t h e b a t t e r y t o t h e P M U

, a n d t h e n w a t c h t h e L E D

, i f y o u c a n s e e t h e L E D b l i n k s ( )

, t h e s y s t e m i s w o r k i n g

. A E T R U M C

A E T R U M C 

### T r a d i t i o n a l R e c e i v e r

P o w e r S u p p l y S

- B u s / S

- B u s 2 / P P M R e c e i v e r N o t e : T h e N A Z A

- M V 2 f l i g h t c o n t r o l s y s t e m d o e s n ' t s u p p o r t G i m b a l f u n c t i o n w h e n u s e d o n t h e O c t o

- r o t o r a i r c r a f t

. F o r b i g a i r c r a f t t h a t i s l a r g e r t h a n 6 5 0 o r w i t h h e a v y l o a d

, W K M i s r e c o m m e n d e d

.

### © 201 5 DJI . All Rights Reserved. 

## 7 | 

# Assistant Software Installation and Configuration
Step1 Software and Driver Installation

Installing and running on Windows

1. Plea se download the driver and the A ssi stant installation software in EXE format from www.dji.com

.
2. S witch on the transmitter and then power on your autopilot system.

3. Connect your autopilot system and PC via a Micro

- USB cable

.
4. Open the driver installation software and follow the instructions to complete installation

.
5. Run the Assistant installation software and follow the instru ctions to complete installation

.

The installer in EXE format is supported on Wi n XP, Win7, Win8 (32 or 64 bit)

.

Installing and running on Mac OS X

1. Download the Assistant installer in DMG format from the download page of NAZA

- M V2 on the DJI

website.

2. Run the installation software and follow the prompts to finish installation.

3. When launching for the first time if use Launchpad to run the NAZA

- M V2 Assistant Software, Launchpad

won’t allow access because the software has not been reviewed by Mac App Store.

### © 201 5 DJI . All Rights Reserved. 

## 8 | 4. Locate the NAZA

- M V2 icon in the Finder and open the file by Control or right clicking the icon and

selecting “Open” from the menu.

5. After the first successful launch, double

- clicking the NAZA

- M V2 ic on in the Finder or using Launchpad

will open the application.

Installer in DMG format is support ed on Mac OS X 10.6 or above.

The NAZA

- M V2 Assistant on Mac OS X and Windows are exactly the same. The Assistant appear in

other places of this manual is based on Windows version.



# Step 2

Configuration by Assistant on a PC

1. Power on the PC. Make sure your computer is connected to the Internet for the first t ime you use.

2. Switch on the transmitter first, and then power on the autopilot system. Connect the autopilot system to

the PC with a Micro

- USB cable. DO NOT break the connection until setup is finished.

3. Run the Assistant Software.

4. Observe the indicators on the left bottom of the software. ( They are the connection indicator and communication indicator in order.) If the communication indicator is blinking, that the software is ready,

please go to next step.

5. Select the “Info” option. Check the software firmwa re version. If the upgrade is available, you may update

the assistant software.

### © 201 5 DJI . All Rights Reserved. 

## 9 | 6. Select the “Upgrade” option. Check the Main Controller, GPS and IMU firmware version.

7. Select the “Basic” option. Please follow step

- by

- step for your first

- time

- configuration. B asic configuration
is necessary, including Mixer Type, Mounting, RC, and Gain settings.

8. You can click the “Advanced” option for more parameter settings. Advanced setting is optional. There are
settings of Motor, FailSafe, Intelligent Orientation Control (I OC), Gimbal, Low

- Voltage Alert, and Flight

Limits. Read the instruction in the assistant software to obtain more details.

9. Select the “Viewer” option to check all parameters.

10. Then break the Micro

- USB cable, power off the aircraft. Finished.

(1) You may be required to fill register information for your first

- time

- usage.
(2) If the communication indicator is blue on, please double check the connections.

(3) Basic configuration is necessary before you go to the “Basic Flying Test”

. (4) U sers are required to install a Win dows system , since the software can only run on Windows

system

. 

## (1) If the firmware upgrade is available, please upgrade it by referring to the Firmware Upgrade

in the Appendix.


## (2) This step is required to use together with the assistant software to obtain mo re details. 

## Configuration Information

Recommended Parameters A ircraft Configuration Information

Motor ESC Propeller Battery Weight

S900 DJI

- 4216 DJI

- 40A Z

- BLADE

- 17 × 6 .0 Inch 6S

- 12000 6800g

F450 DJI

- 2312 DJI

- 20A Z

- BLADE

- 9.4 × 5 .0 Inch 4S

- 5000 890g

F550 DJI

- 2312 DJI

- 20A Z

- B LADE

- 9.4 × 5 .0 Inch 4S

- 5000 1530g

A ircraft Basic Gain Attitude Gain M ax Angular Rate

Pitch Roll Yaw Vertical Pitch Roll Pitch Roll

S900 100 100 100 100 160 160 220 220

F450 95 95 70 100 100 100 300 300

F550 110 100 80 100 100 1 00 300 300

### © 201 5 DJI . All Rights Reserved. 

## 10 | 

# Basic Flying
Control Mode Knowledge
Please read the Control Mode Knowledge clearly before usage, to know how to control the aircraft.

Different control modes will give you different flight performances. Please make sure you understand the fe atures

and differences of the three control modes.

GPS ATTI. Mode
( With GPS Module ) ATTI. Mode Manual Mode

Rudder Angular Velocity Maximum rudder angular velocity is 150°/s

Command Linearity YES

Command Stick Meaning Multi attitude control; Stick cente r position for 0 ̊ attitude, its endpoint is 35 ̊. Max

- angular velocity is 150°/s.
No attitude angle limitation

and vertical velocity locking.

Altitude Lock Maintain the altitude best above 1 meter from ground. NO

Stick Released Lock position if GPS signal
is adequate. Only attitude stabilizing. NOT Recommend

GPS Lost When GPS signal has been
lost for 3s, system enters ATTI. Mode automatically. Only performing attitude
stabilizing without
position lock. ---

Safety Attitude & speed mixture control ensures stability
Depends on experience. Enhanced Fail

- Safe(Position lock when hovering) Auto Level Fail

- Safe (Attitude stabilizing) With GPS/Compass module and the failsafe requirements are satisfied, in each Control Mode (including GPS Mode, ATTI. Mode, Man ual Mode and IOC Mode), the aircraft will

enter the failsafe Mode.
Applications AP work Sports flying.

---



# Start & Stop Motor Knowledge

(1) Both Immediately Mode and Intelligent Mode are available in the Assistant Software:

Advanced

- >Motor

- >Stop Type.
(2) Sto p Motor method is defaulted to Immediately Mode

. Please get to know well about this section before flying.

1 Start Motor : Pushing throttle stick before takeoff will not start the motors. You have to execute any one of

following four Combination Stick Comman ds (CSC) to start the motors:

### © 201 5 DJI . All Rights Reserved. 

## 11 | 2 Stop Motor : We provide two options to stop motors in the assistant software : Imm ediately and Intelligent.

(1) Immedia tely Mode: If you select this mode, in any control mode, once motors start and throttle stick is

over 10%, motors will not stop immediately only when throttle stick is back under 10% the motors will

stop. In this case, if you push the throttle stick over 1 0% within 5 seconds after motors stop, motors

will re

- start, CSC is not needed. If you don’t push throttle stick after motors start in three seconds,

motors will stop automatically.

(2) Intelligent Mode: By using this mode, different control mode has different way of stopping motors. In

Manual Mode, only executing CSC can stop motors. In A TTI. Mode or GPS ATTI . Mode, any one of

following four cases will stop motors:

a) You don’t push throttle stick after motors start within three seconds;

b) Executing CSC;

c) Throttle s tick under 10 %, and after landing for more than 3 seconds.

d) If the angle of multi

- rotor is over 70°, and throttle stick under 10%.



# Notes of Intelligent Mode

(1) In ATTI. / GPS ATTI. Mode, it has landing judgment, which will stop motors.

(2) Start motors in ATTI. / GPS ATTI. Mode, you have to execute CSC and then push throttle stick

over 10% in 3 seconds, otherwise motors will stop after 3 seconds.

(3) During normal flight, only pull throttle stick under 10% will not stop motors in any control mode.

(4) For safety reason, when the slope angle of multi

- rotor is over 70° during the flight in ATTI. /

GPS ATTI. Mode (may be caused by collision, motor and ESC error or propeller broken down),

and throttle stick is under 10%, motors will stop automatically. 

# Notes of Intelligent Mode & Immediately Mode

(1) If you choose the Immediately Mode , you should not pull throttle stick under 10% during flight,

because it will stop motors. If you do it accidentally, you should push the throttle stick over 10%

in 5s to re

- start motors.

(2) DO NOT e xecute the CSC during normal flight without any reason, or it will stop motors at

once.
(1) If you choose the Intelligent mode, and the throttle stick is under 10%, this will trigger the

landing Procedure, in any control mode. In this judgment, pitch, roll and yaw controls are denied

except the throttle, but multi

- rotor will still auto level.

(2) In any control mode, DO NOT pull throttle stick under 10% during normal flight without any

reason.

(1) Any of these two cut off types will only work properly if T X calib ration is correct done.

(2) In failed

- safe, CSC is denied by the main controller, motors will hold their state.

### © 201 5 DJI . All Rights Reserved. 

## 12 | 

# Step 

# 1 Compass Calibration

Without GPS module, please skip this step. If you use w ith GPS module, follow step

- by

- step for calibration.

(1) DO NOT cali brate your compass where there is magnetic interference, such as magnetite, car
park, and steel reinforcement under the ground.
(2) DO NOT carry ferromagnetic materials with you during calibration, such as keys or cell phones.
(3) Compass module CANNOT work in the polar circle.

(4) Compass Calibration is very important, otherwise the system will work abnormal.



# Calibration Procedures

1. Switch on the transmitter, and then power on autopilot system!

2. Quickly switch the control mode switch from GPS Mode to Manual Mode and b ack to GPS Mode (or

from GPS Mode to ATTI. Mode and back to GPS Mode ) for more than 5 times, The LED indicator will

turn on constantly yellow so that the aircraft is ready for the calibration

. 3. (Fig.1) Hold your Multi

- rotor horizontal and r otate it around t he gravitational force line (about 360 o 

## ) until
the LED changes to constant green, and then go to the next step.

4. (Fig.2) Hold your Multi

- rotor vertically and rotate it ( its nose is downward ) around the gravitational force

line (about 360 o 

## ) until the LED turn s off, meaning the calibration is finished

.

Fig.1 Fig.2

5. If the calibration was successful, calibration mode will exit automatically. If the LED keeps flashing quickl y
Red, the calibration has failed. Switch the control mode switch one time to cancel the calibration, and

then re

- start from step 2.

(1) When the GPS is abnormal, the Main controller will tell you by the LED blinking Red and Yellow

alternately ( ), disable the GPS Module, and automatically enter the aircraft into the

ATTI. Mode.

(2) You don’t need to rotate your multi

- rotor on a precise horizontal or vertical surface, but keep at

least 45° difference between horizontal and vertical calibration.

(3) If you keep having calibration failure, it might suggest that there is very strong magnetic
interference around the GPS /Compass module, please avoid flying in this area.

(4) When to do re

- calibration

a) The flight field is changed.
b) When the multi

- rotor mechanical setup has changed:

z If the GPS/Compass module is re

- positioned.

z If electronic devices are added/removed/ re

- positioned (Main Controller, servos,
batteries, etc.).

z When the mechanical structure of the multi

- rotor is changed.

### © 201 5 DJI . All Rights Reserved. 

## 13 | c) If th e flight direction appears to be shifting (meaning the multi

- rotor doesn’t “fly straight”).
d) The LED indicator often indicates abnormality blinking when the multi

- rotor spins. (It is normal for this to happen only occasionally)



# Step 

# 2 Assembly Checking Lis t Please check each item, to make sure for safety.

Any of the following mistakes will lead to a dangerous accident, double check all these items:

(1) Rotation direction of motor is opposite

(2) Infirm connection between the motor and the ESC

(3) Wrong or infirm i nstallation of Main controller

(4) Wrong or infirm connection between the main controller and ESC.

(5) Propeller installation mistak e
(6) M agnetiz ation of t he compass
Make sure the following items are correct.

(1) Make sure you have assembled your multi

- rotor correctl y.
(2) Make sure you have done the configuration procedure correctly.

(3) Make sure all connections are in good condition.

(4) Make sure batteries are fully charged for your transmitter, autopilot system and all devices.



# Step 

# 3 Before Flight
Carry out the following p rocedures (is based on Intelligent Mode of Motor Stop) to make sure all
configurations are correct. Refer to the Appendix

- >LED Description for more LED details.

1. Always switch on the transmitter first, then power on multi

- rotor!

2. Keep the aircraft stationa ry until the system start and self

- check has finished ( )

. After that, the LED may blink Yellow 4 times quickly ( )

. Start motor is disable during LED blink ing

Yellow 4 tim es quickly ( ) , as the system is warm ing up

.
3. After the 4 times Yellow LED disappear s, t oggle the control mode switch on your transmitter to make sure it

is working properly. For examp le, LED blinks ( ), which means the system is in ATTI. Mode and the

GPS s ignal is worst Check it with LED indicator to specify the current working mode for MC. See following

table for details about LED indicator;

(1) There are Manual Mode and ATTI. Mode without a GPS /Compass module, no GPS signal status LED

indicator.
(2) After connect ing to the GPS /Compass module, GPS ATTI. Mode is available , and GPS signal status

LED indicator is available

.

### © 201 5 DJI . All Rights Reserved. 

## 14 | Control Mode LED I ndicator GPS Signal Status LED Indicator

Manual Mode: NO LED

ATTI. Mode: ( indicates that is stick(s) not at center)

GPS Mode : ( indicates that is stick(s) not at center ) Signal is best ( GPS satellites > 6 ) : NO LED

Signal is well ( GPS satellites = 6 ) : Signal is bad ( GPS satellites = 5 ) : Signal is worst ( GPS satellites< 5 ) :

4. Keep the aircraft stationary, and then push both sticks to the left bottom or right bottom (shown as the

following chart , defined as Combi nation Stick Commands (CSC) ), to start the motors.

5. Release the yaw, roll and pitch sticks and keep them at the mid point

, and the throttl e stick under the mid

point

. T hen check whether all propellers are rotating correctly.

6. Stop motors, power off the Multi

- rotor

.
7. Make sure all settings and configurations are correct and then you can take off you aircraft.



## After power on , if abnormal LED In dicator occurs, please refer to the Abnormal LED instruction in the FAQ and

aids troubleshooting.



# Step 

# 4 Flying Test

1. Choose an open space without obstruction, tall buildings and crowds as flying filed. Place the aircraft 3

meters away from you and others, to avoid accidental injury.

2. If in GPS ATTI. Mode, place the aircraft in an open space without buildings or trees. Take off the aircraft
after 6 or more GPS satellites are found (Red LED blinks once or no blinking). If in Manual Mode or ATTI.

Mode, you can skip this step.

3. Start

- up (1) S witch on the transmitter first, then power on multi

- rotor! Keep the aircraft stationary until the

system start and self

- check has finished.

(2) Please wait for the system to warm up gradually with the LED blinks Yellow 4 times quickl y
( ). You should not start the motors until the blinking disappears.

(3) Keep the aircraft stationary, and execute the CSC to start the motors.

(4) Release the yaw, roll and pitch sticks and keep them at the mid point , at the same time raise the

throttle stick from the bottom. The motors will stop if you do not push the throttle stick from the

bottom within 3 sec and you will need to re

- start the motors.

(5) Keep raising the throttle stick until all the rotors are working, pu sh the throttle stick to the mid point

and then take

- off your multi

- rotor gently, pay attention not to push the stick excessively.

### © 201 5 DJI . All Rights Reserved. 

## 15 | (6) Pay attention to the aircraft movement at any time when flying, and use the sticks to adjust the

aircraft’s position. Keep th e yaw, roll, pitch and throttle sticks at the mid point to hover the aircraft

at the desired height.



# 4. Lower the aircraft slowly. Pull the throttle stick to the bottom and then execute the CSC to stop the motors

after landing.


# 5. Please always power off the Mu lti

- rotor first, and then switch off the transmitter after landing.



# FLYING NOTES(VERY IMPORTANT) !!!

(1) If the warm up waiting is longer than 2 minutes (the 4 times Yellow blink c ontinue s ), please power

off for 10 minutes, cold start, and then connect the assistant software, enter the "Tools"

- > IMU

calibration, carry out t he Advanced calibration.

(2) I f you enable the Immediately Mode of Motor Stop ; you should not pull throttle stick under 10%

during flight, because it will stop motors. If you do it accidentally, you should push the throttle

stick over 10% in 5s to re

- start mot ors.
(3) DO NOT execute the CSC during normal flight without any reason, or it will stop motors at once.

(4) Pay attention to the GPS satellite status LED indicator. Bad GPS signal may lead the aircraft to

drift when hovering.

(5) DO NOT fly near to ferromagnetic sub stances, to avoid strong magnetic interference with the

GPS.

(6) Please avoid using GPS ATTI. Mode in the areas, where GP S signal is most likely bad

. (7) If the LED flashes quickly Red then this indicates battery voltage is low, land ASAP.

(8) If the transmitter indic ates low

- battery alarm, please land ASAP. In this condition the transmitter

may cause the aircraft to go out of control or even crash.

(9) In GPS ATTI. Mode, make sure that the home point is recorded when the GPS signal is well;

otherwise the home point recor ding may be not so precise.

(1) In ATTI Mode, throttle stick center position is for 0m/s along the vertical direction. You should

keep the position of throttle stick higher than 10% from cut

- throttle during the flight! In any

control mode, DO NOT pull throt tle stick under 10% during normal flight without any reason.

(2) It is recommended to land the aircraft slowly, to prevent the aircraft from damage when landing.

(3) If Low

- Voltage Alarm is set, the aircraft will act according to the configuration of the Assistant

Software once Low

- Voltage Alarm is triggered. Make sure you remember what you have set

before.
(4) If Fail

- Safe function is set, the aircraft will act according to the configuration of the Assistant

Software once Fail

- Safe is triggered. Make sure you remember what you have set before.

### © 201 5 DJI . All Rights Reserved. 

## 16 | 

# Advanced Functions

A



# 1 FailSafe

An introduction of Go

- Home and Landing.



# 1 R e c o r d H o m e P o i n t

H o m e P o i n t


# 2 T x 

# 3 T x



# 5 T x S i g n a l l o s t

T x M u l t i

- r o t o r



# 4 T x S i g n a l l o s t > 3 s S t a y h o v e r

R e a d y t o G o - H o m e

C u r r e n t l o c a t i o n ≤ 2 0 m C u r r e n t l o c a t i o n > 2 0 m



# 6 G r o u n d

2 0 m A s c e n d f i r s t H o v e r 1 5 s , t h e n l a n d G o - H o m e G o - H o m e



## Home

- point: Before takeoff, current position of multi

- rotor will be saved as home

- point by MC automatically when

you start the motors for the first time after 6 or more GPS satellites are found (red light blinks once or no blinking)

for 10 seconds.

(1) Please make sure to record the home

- point before takeoff, and clearly know where it is.
(2) During go

- home the nose direction of the aircraft is facing toward the home

- point, the aircraft is

flying directly from the current position to the home

- point.
(3) You can regain the control during the aircraft is hovering 15 seconds.

T h e f l o w c h a r t o f f a i l s a f e a n d h o w t o r e g a i n c o n t r o l

( 2 ) T u r n o f f t h e T X ( w e a s s u m e y o u w a n t t o t r i g g e r f a i l s a f e ) ( 1 ) T h e a i r c r a f t f l i e s f a r a w a y , T X i s o n b u t t h e
s i g n a l i s w e a k

. A t t i t u d e M o d e : I n A t t i t u d e M o d e a s
s o o n a s y o u g e t s i g n a l y o u c a n
r e g a i n c o n t r o l

.

G P S M o d e : s w i t c h t h e T X m o d e
s w i t c h t o A T T I

, i f t h e r e c e i v e r i s
c o n n e c t e d

, t h e n y o u w i l l r e g a i n
c o n t r o l

. A t t i t u d e M o d e : ( 1 ) t h e a i r c r a f t w i l l l e v e l i t s a t t i t u d e i m m e d i a t e l y ( 2 ) 3 s e c o n d s l a t e r , f a i l s a f e i s t r i g g e r e d a n d

a i r c r a f t w i l l s t a r t t o g o h o m e

. ( 3 ) I f s i g n a l i s r e g a i n e d d u r i n g ( 1 ) o r ( 2 )

, i t w i l l r e s u m e n o r m a l f l i g h t i m m e d i a t e l y

.

G P S M o d e : ( 1 ) t h e a i r c r a f t w i l l s l o w d o w n a n d h o v e r

. ( 2 ) i f t h e s i g n a l i s r e s t o r e d w i t h i n 3 s e c o n d s ( T X a n d r e c e i v e r
c o n n e c t e d )

, t h e s y s t e m w i l l i m m e d i a t e l y r e t u r n t o n o r m a l

o p e r a t i o n ; d o e s n o t e n t e r f a i l s a f e

. ( 3 ) i f n o t r e c o n n e c t e d

w i t h i n 3 s e c , t h e s y s t e m w i l l e n t e r f a i l s a f e , t h e n e v e n i f t h e
s i g n a l i s r e s t o r e d

, t h e s y s t e m w i l l n o t e x i t f a i l s a f e

.

W e s t r o n g l y r e c o m m e n d y o u D O N O T t r y t h i s , b e c a u s e t h e r e a r e t h r e e t y p e s o f r i s k : ( 1 ) Y o u m u s t b e p r e t t y c l e a r w h e t h e r t h e H o m e

- p o i n t i s O K f o r l a n d i n g o r
n o t

. ( Y o u h a v e t o u n d e r s t a n d t h e d e f i n i t i o n o f H o m e

- p o i n t w e l l a n d t h e
w o r k i n g p r o c e s s o f f a i l s a f e ) ( 2 ) I f t h e r e a r e t a l l b u i l d i n g s a r o u n d

, t h e a i r c r a f t m a y b e o b s t r u c t e d o n t h e
w a y

. ( 3 ) W h e n G P S s i g n a l i s b a d o r G P S i s n o t w o r k i n g , f a i l s a f e w i l l n o t w o r k

. I n t h i s c a s e , t h e b e h a v i o r o f t h e a i r c r a f t i s t h e s a m e a s i n t h e a b o v e c o n d i t i o n

. I f y o u w a n t t h e a i r c r a f t t o R e t u r n H o m e , p l e a s e d o n o t t u r n t h e T X b a c k o n w i t h i n 3 s e c o n d s *

, o t h e r w i s e t h e a i r c r a f t

w i l l e x i t f a i l s a f e m o d e i m m e d i a t e l y

.

W h e n y o u t u r n o f f t h e T X

, u s e t h e f o l l o w i n g
m e t h o d t o r e g a i n c o n t r o l : ( 1 ) S w i t c h t h e T X s w i t c h t o G P S

. ( 2 ) a n d t h e n p u t t h r o t t l e t o t h e c e n t e r p o s i t i o n ( g r e a t e r t h a n 3 s e c a f t e r s w i t c h i n g o f f

, i m p o r t a n t )

, y o u c a n n o w t u r n t h e T X b a c k o n

. ( 3 ) t h e n y o u c a n s w i t c h t h e T X C o n t r o l m o d e
s w i t c h t o A T T I t o r e g a i n c o n t r o l

. I f y o u c h o o s e t o t u r n o f f t h e T X

, y o u m u s t b e p r e t t y s u r e t h a t y o u k n o w h o w t o r e g a i n c o n t r o l

. H e r e
w e o f f e r a m e t h o d

, p l e a s e r e a d

c a r e f u l l y

. 

### T h i s s e c t i o n w i l l d e m o n s t r a t e t h e w o r k i n g l o g i c o f f a i l s a f e a n d h o w t o r e g a i n c o n t r o l

. T h e f o l l o w i n g d e s c r i p t i o n i s e f f e c t i v e o n l y w h e n : 1

. T h e a i r c r a f t i s i n f l i g h t

. 2

. T h e G P S w o r k s n o r m a l l y a n d s i g n a l i s g o o d ( ≥ 6 s a t e l l i t e , t h e L E D b l i n k s a s i n g l e
r e d l i g h t o r n o r e d l i g h t )

.

N o t e : i f y o u s t a r t t h e m o t o r s , b u t d o n o t p u s h t h e t h r o t t l e t o t a k e

- o f f t h e a i r c r a f t
, i n t h i s c a s e i t i s v e r y d a n g e r o u s t o t u r n
o f f t h e T X

, b e c a u s e t h e a i r c r a f t w i l l t a k e o f f a u t o m a t i c a l l y , s o d o n o t t r y t h i s

. T h e a i r c r a f t b e h a v i o r
a f t e r f a i l s a f e H o w t o r e g a i n c o n t r o l
P r e c a u t i o n s W h a t t r i g g e r e d f a i l s a f e

* I f s i g n a l l o s t f o r m o r e t h a n 3 s e c o n d s f a i l s a f e w i l l b e t r i g g e r e d

, i f s i g n a l r e g a i n e d w i t h i n 3 s e c o n d s i t w i l l e x i t f a i l s a f e i m m e d i a t e l y

.

### © 201 5 DJI . All Rights Reserved. 

## 17 | 

# A



# 2 Low

- Voltage Alert

In order to pre vent your multi

- rotor from a crash or other harmful consequences caused by low battery voltage,

there are two levels of low voltage protection available to use. You can choose to use or not to use them; however

we strongly recommend using the protections i f available! Low

- Voltage Alert is to indicate that the battery cannot
provide enough power for the aircraft, in order to warn you to land the aircraft ASAP. You can configure this

function in the assistant software, and please read the text in the software carefully before your flight. Make sure to

carry out the Current Voltage Calibration.

There are both first level and second level protections. The first level protection has LED warning. During second

level protection the aircraft will land automatically with LED warning. Meanwhile the center point of throttle stick

will move up slowly to 90% of endpoint, you should land ASAP to prevent your aircraft from crashing!

It is not for fun, you should land your aircraft ASAP to prevent your aircraft from crashin g or other harmful

consequences!!!

(1) Configure the FailSafe function in the assistant software

- > “Advanced”

- > “F/S” and read the

instruction thoroughly and carefully.

(2) Configure the Low

- Voltage Alert function in the assistant software

- > “Advanced”

- > “V oltage”

and read the instruction thoroughly and carefully.

### © 201 5 DJI . All Rights Reserved. 

## 18 | 

# A



# 3 Intelligent Orientation Control (IOC) Flight (with GPS module)

Definition of Forward Direction:



## Multi

- rotor will fly along this direction when you push the elevator stick ( ). 

# Step 

# 1 Before You Start

Usually, the forward direction of a flying multi

- rotor is the same as the nose direction. By using IOC, wherever the

nose points, the forward direction has nothing to do with nose direction. The red and blue arrows on th e transmitter

are corresponding to pitch and roll operations in the following diagram.

z In course lock flying, the forward direction is the same as a recorded nose direction. All the following

requirements are met: the autopilot system is in ATTI. Mode or G PS ATTI. Mode.

Normal flying Course Lock Flying

z In home lock flying, the forward direction is the same as the direction from home point to multi

- rotor. All the

following requirements are met: 6 or more GPS satellites a re found, in GPS ATTI. Mode, and the aircraft is

further than 10m away from the home point.

Normal flying Home Lock Flying 

# Step 

# 2 IOC Switch Setting

Before using the IOC function, you have to choose a 3

- position switch on your transmitter as the IOC switch, which

is also used for recording the orientation, home position in corresponding modes. Refer to the assistant software;

click the “Advanced” to find the “IOC”.

IOC Switch

IOC Function OFF Course Lock H ome Lock

The above table is for example. The function of the switch position may be reversed since the
normal/reversed setting of the switch channel. Toggle the switch and observe the slider position of

channel X2 on the assistant software screen, the corresponding area should turn blue.

### © 201 5 DJI . All Rights Reserved. 

## 19 | 

# Step 

# 3 Method of Forward Direction and Home Point Recording

If you use the IOC function, please be aware of the Forward Direction of Course Lock Flying, and the home point of

Home Lock Flying. There are two ways to reco rd the forward direction and the home point : Manually and

Automatically. You may choose any one record method. The LED will blink Green quickly if successfully recorded.

Course Lock Home Lock

Automatically 30 seconds after you power on the
autopilot sys tem. Before takeoff, the current position of the aircraft
will be saved as home point when you start the

motors for the first time after 6 or more GPS

satellites have been found for 10 seconds.

Manually 30 seconds after you power on the
autopilot system. Toggle the IOC switch
from Off to Course Lock, and back to Off
quickly 3 to 5 times. After 6 or more GPS satellites have been found.

A nd the aircraft can be hovering. Toggle the IOC
switch from Course Lock to Home Lock, and back
to Course Lock quickly 3 t o 5 times.
DO NOT toggle the switch between Off to Home Lock, since it may change the recording of the

Forward Direction of Course Lock

. 

# Step 

# 4 IOC Flying Test

Then you can do Course Lock and Home Lock flying test

. Carry out an IOC flight by the followi ng procedure. The Control Mode LED will blink Yellow and Green

alternatively ( ) to indicate the IOC mode only when the main controller is really to fly in Course Lock, Home

Lock modes.

During the same flight STEP1 : Record STEP2: ON STEP3: OFF STEP4: ON again

Course Lock

Switch Setting Record the

Forward

Direction Set Control Mode switch at GPS or ATTI. position,
Toggle IOC switch from OFF
to Course Lock position Toggle IOC switch
to OFF position Toggle I OC switch

from OFF to Course
Lock position

Home Lock

Switch Setting Record the

Home Point Set Control Mode switch at GPS position,
Toggle IOC switch from OFF
to Home Lock position Toggle IOC switch
to OFF position Toggle IOC switch

from OFF to Ho me Lock position

Aircraft moving direction when pull pitch stick Aircraft moving direction when pull roll stick

Home point Aircraft ( th e arrow is pointing to the direction of the aircraft nose )

### © 201 5 DJI . All Rights Reserved. 

## 20 | IOC FLYING NOTES !!!

(1) When Multi

- rotor is flying by home lock far away from you and the home point, please DO NOT

toggle the IOC switch many times quickly so as to avoid the change of home point wi thout your

attention.

(1) Home lock flying requires that 6 or more GPS satellites are found and the aircraft is further than

10m away from the home point.

(2) If the IOC flying requirement is not satisfied, the autopilot system will quit IOC control mode.

Pleas e be aware of the LED indicator, to know the current control mode of the autopilot system.

(1) Blinking indications of IOC are:
a) Before motors start: blink, all sticks (except throttle stick) return to center; blink, stick(s) (except throttle stick) not at center.

b) After motors start and throttle stick is over 10% in 3 seconds: blink, all sticks return

to center; bli nk, stick(s) not at center.
(2) Before you do the home lock flight, you have to fly the aircraft out of the 10m range around

home point, and then flip the IOC switch to Home Lock position to fly in home lock when all the

requirements are met. If you have alrea dy toggled the IOC switch to Home Lock position when

the aircraft is still in 10m range around home point, and this is the first time you are going to fly

in home lock during the current flight, then if all the requirements are met, the main controller

wil l change into home lock automatically when Multi

- rotor flies out the 10m range around home

point.

(3) When flying in Home Lock mode, if any of the following situations happen, then the system will

quit Home Lock flying and automatically enter Course Lock flyin g. The aircraft will fly in Course

Lock using the earlier forward direction.

a) The aircraft fly’s within 10m range of the home point.

b) You toggle the control mode switch to the ATTI. Mode.

c) The GPS signal becomes bad (The GPS signal LED is blinking Red twice o r three times).

(4) We suggest that you should know clearly which flight lock method you are going to fly, and you

know the locked forward direction or home point, before you switch on IOC mode during the

flight.

### © 201 5 DJI . All Rights Reserved. 

## 21 | 

# A



# 4 Receiver Advanced Protection Function

Y ou are asked to enable this function by connecting to the Assistant Software, please set it at the section of

Basic

- >R/C

- > Receiver Advanced Protection.

If you choose enable it, the FailSafe will be triggered if the following situations occur during flight

. According to the differen ce of the aircraft height, there are two situations.

1. Lower than 100m, the A/E/R channel is not at the mid point

.
2. Higher than 100m, the A/E/R channel is not at the mid point or the throttle stick is above the mid point

.
I n the GPS Mode or ATTI. Mode, if the requirement a) or b) is satisfied, and the output data of four channels

A/E/R/T h ave not changed for 20 seconds, then the aircraft will hover automatically. A fter that, if the output data

of four channels A/E/R/T still do not an y change s and last for 10 seconds, the autopilot system will think that the

data from receiver is abnormal, and then enter the FailSafe Mode.

Brief introduction of how to quit the FailSafe Mode

If there is any command change from the receiver, the autopil ot system thinks that the receiver is regained. I n ATTI.

Mode and Manual Mode, it will quit the FailSafe Mode automatically

. I n GPS Mode, please toggle the control mode

switch to the ATTI. Mode and Manual Mode position to regain the control. Refer to the F ailSafe section for more

details.

### © 201 5 DJI . All Rights Reserved. 

## 22 | 

# A5 Flight Limits

T he flight limits function is default enabled in the NAZA

- M Flight control system, it ’ s aimed to restrict the flying

height and distance of the aircraft. T he Max Height restricts the vert ical distance between the aircraft and the

Home point, the Max Radius restricts the horizontal distance between the aircraft and the Home point.

T he default Max Height is 2000m and Max Radius is 2000m

. U sers can write the values of the Max Height and Max

R adius in the Assistant software, t he range of the Max Height is 10m

- 100000m, the range of the Max Radius is the

same. S o that the aircraft will fly in the entered range, which is a cylinder space above the Home point.

(1) Heigh t Limit work s when the contr ol mode is GPS or ATTI. Mode

. Radius Limit work s when the

control mode is GPS and the s atellite number ≥6

. (2) If the aircraft flies out of the limits, it's still controllable except flying further away.

(3) If the control mode is changed to GPS when the aircraft is out of Max Radius, the aircraft will fl y
back within the entered range

. (4) The Failsafe and the Ground Station operations are not restricted to the Flight Limits.

### © 201 5 DJI . All Rights Reserved. 

## 23 | 

# Appendix
Specifications

General

Built

- In Functions (1) Three Modes of Autopilot

(2) Enhanced Fa il Safe

(3) Low Voltage Protection (4) S

- Bus / S

- Bus 2 Receiver Support

(5) PPM Receiver Support

(6) 2

- axle Gimbal Support 

# Peripheral

Supported Multi

- rotor z Quad

- rotor I4, X4;

z Hexa

- rotor I 6, X6, IY6, Y6.

z Octo

- rotor I 8

, V 8

, X 8

Supported ESC output 400Hz refres h frequency.

Recommended Transmitter PCM or 2.4GHz with a minimum 4 channels.

Assistant Software System Requirement Windows XP SP3; Windows 7; Windows 8 

# Electrical & Mechanical

Working Voltage Range z MC: 4.8V ~ 5.5 V

z PMU Input: 7. 4 V ~ 26.0 V (recomme nd 2S ~ 6S LiPo) Output( V

- SEN port red wire ): 3A@5V Output( V

- SEN port red wire )burst current:7.5A Power Consumption z MAX: 1.5W(0.3A@5V)

z Normal: 0.6W(0.12A@5V)

Operating Temperature

- 10°C ~ 50°C (14F ~122F)

Weight z MC: 27g

z GPS/Compass: 27g

z PMU : 28g

z LED: 13g

Dimensions z MC: 45.5mm × 32.5mm × 18.5mm

z GPS/Compass: 46mm (diameter) x 10mm

z PMU : 39.5mm × 27.5mm × 10.0mm

z LED : 25mm × 25mm × 7.0mm 

# Flight Performance (can be effected by mechanical performance and payloads) Hovering Accuracy (GPS Mode) z Ve rtical: ± ± 0.8m

z Horizontal: ± ± 2.5m
Max Yaw Angular Velocity 200°/s

Max Tilt Angle 3 5°
Max Ascent / Descent Speed Ascent : 6m/s

, Descent : 4.5 m/s

### © 201 5 DJI . All Rights Reserved. 

## 24 | 

# MC/ PMU Firmware Upgrade
Please follow the procedure for software and firmware upgrade; otherwise the sy stem might not work properly. F or

SAFETY REASONS, DO NOT use power battery during firmware upgrade.

1. Make sure your computer is connected to the Internet.

2. Please close all the other applications during the firmware upgrade, including anti

- virus software and

firewall.

3. Make sure the power supply is securely connected. DO NOT un

- plug the power supply until firmware

upgrade has finished.

4. Connect system to PC with Micro

- USB cable, DO NOT break connection until firmware upgrade is

finished.

5. Run Software and wait f or connection.

6. Select Upgrade option Æ Check the MC and PMU Firmware Version

.
7. DJI server will check your current firmware version, and get the latest firmware prepared for the unit.

8. If there is a firmware version more up

- to

- date than your current version, yo u will be able to click to
update them.

9. Wait until Assistant software shows “finished”.

10. Click OK and power cycle the unit after at le ast 5 seconds.

11. Your unit is now up

- to

- date.

(1) After firmware upgrade, please re

- configure the system using Assistant so ftware.
(2) If firmware upgrade failed, the system will enter waiting for firmware upgrade status

automatically, please try again with the above procedures.

(3) Select Upgrade option Æ Check the GPS Firmware Version, online upgrade is disable

.

### © 201 5 DJI . All Rights Reserved. 

## 25 | 

# LED Descri ption System Status LED Flashing

System start and self

- check

IMU abnormal data or need a dvanced

c alibration*

W arm up after power on

T he aircraft is moved or b ias of s ensors too b ig

Compass e rror too b ig

, need recalibration.

T ransmitter (TX) signal lost , enter the FailSafe.

TX stick(s) mid point error too big

Low v oltage a lert or other abnormal alert*
(e.g. Configuration error, TX data error, Enable

low v oltage protection without PMU, SN error

or Compass abnor mal work

. )

Record forward direction or home point

Control Mode Indictor Manual Mode : None

ATTI. Mode : ( stick(s) not at cen ter )

GPS Mode : ( stick(s) not at center )

IOC Mode : ( stick(s) not at center )

GPS Signal State Indicator ( GPS/Compass Module is necessary ) GPS Signal is Best( GPS Satellite number > 6 ) : None GPS Signal is Well( GPS Satellite number = 6 ) : GPS Signal is Bad ( GPS Satellite number = 5 ) : GPS Signal is Worst ( GPS Satellite number < 5 ) :



# Compass Calibration LED Flashing

Begin horizontal calibration

Begin vertical calibration

Calibration or others error

* You can f igure out the error by connecting the autopilot system to the assistant software

.

### © 201 5 DJI . All Rights Reserved. 

## 26 | 

# Instruction of V1 ( also known as NAZA

- M )

V1 ( also known a s NAZA

- M ) system is different from V2 system, if you are V1 system user, please read the following

text carefully

, and refer to the other text in this Guide for usage details (including Assistant Software C onfiguration

, Basic fly ing

, Advanced F unction Appe ndix and FAQ, etc. )

. 

# V

1 Assembly and Connection
Connect the V1 system according to the following chart

.

接 电 调

接 云 台 R / C R e c e i v e r ( J R ) R U D D

T H R O A I L E E L E V 3

- p o s i t i o n s w i t c h c h a n n e l

R / C R e c e i v e r ( F u t a b a / H i t e c ) 1 2 3 4

F u t a b a S

- B u s / S

- B u s 2 S

- B u s

F 1 F 2



### A i r c r a f t N o s e P P M P P M E S C M 1 M 2 M 3 M 4 M 5 M 6 R

/ C S y s t e m T h e s e a r e e x a m p l e c o n n e c t i o n s

. P l e a s e s e t u p A i l e r o n , E l e v a t o r , T h r o t t l e , R u d d e r c h a n n e l s o n y o u r T X f i r s t

, a n d c h o o s e o n e 3

- p o s i t i o n s s w i t c h / c h a n n e l a s c o n t r o l

m o d e s w i t c h

, t h e n c o n n e c t y o u r

r e c e i v e r t o t h e r i g h t p o r t s o n M C

. V U

· D o n o t m o u n t i t o n a n y o t h e r e l e c t r o n i c d e v i c e s

. M a k e s u r e Y o u

c a n s e e t h e L E D l i g h t d u r i n g t h e f l i g h t

.

· I f u s e w i t h D J I m u l t i

- r o t o r , y o u c a n s o l d e r t h e V U p o w e r c a b l e t o

p o w e r p a d s o n f r a m e b o t t o m b o a r d

. P l e a s e r e f e r t o D J I m u l t i

- r o t o r

m a n u a l f o r d e t a i l s

.

· I f u s e w i t h 3 r d p a r t m u l t i

- r o t o r , y o u c a n m a k e a c o n n e c t e r b y

y o u r s e l f t o c o n n e c t V U

, E S C s a n d b a t t e r y

.

· S u f f i c i e n t a i r f l o w o v e r t h e V U i s h i g h l y r e c o m m e n d e d

.

E S C s , M o t o r s

· M o t o r s a n d E S C s i n D J I m u l t i

- r o t o r k i t a r e r e c o m m e n d e d

.

· P l e a s e m a k e s u r e y o u a r e u s i n g t h e E S C s a n d m o t o r s

r e c o m m e n d e d b y t h e m a n u f a c t u r e r o f y o u r m u l t i r o t o r f i r s t

. N A Z A

o u t p u t i s 4 0 0 H z r e f r e s h f r e q u e n c y

.

· I f y o u u s e 3 r d p a r t y E S C s , p l e a s e m a k e s u r e t h e E S C s t r a v e l

m i d p o i n t i s a t 1 5 2 0 u s

. D O N O T u s e 7 0 0 u s t r a v e l m i d p o i n t E S C

, a s i t m a y l e a d a i r c r a f t t o f l y a w a y o r c a u s e i n j u r y a n d d a m a g e

. A f

t e r c o n n e c t E S C s t o m o t o r s , c a l i b r a t e a l l y o u r E S C s o n e b y o n e t h r o u g h t h e r e c e i v e r d i r e c t l y b e f o r e c o n n e c t t h e m t o y o u r M C

, M a k e s u r e p r o g r a m a l l o f t h e m i n t o G o v e r n o r o f f

, B r e a k o f f a n d N o r m a l S t a r t u p t o g e t b e s t e x p e r i e n c e

.

P i t c h R o l l

M C

· P l e a s e u s e 3 M g u m m e d p a p e r p r o v i d e d T o m o u n t M C

, a n d m o u n t

M C p a r a l l e l t o t h e a i r c r a f t h o r i z o n

.

· T h e o u t p u t p o r t s o f M C ( t h e r i g h t s i d e i n f i g u r e ) s h o u l d p o i n t t o

t h e f r o n t o f m u l t i

- r o t o r

. Y o u ’ d b e t t e r p u t M C a t t h e g r a v i t y
c e n t e r o f m u l t i

- r o t o r

. P l e a s e m a k e s u r e a l l p o r t s a r e a c c e s s i b l e

w h e n i n s t a l l i n g t h e M C s o a s t o f a c i l i t a t e w i r i n g a n d s o f t w a r e
c o n f i g u r a t i o n

.

· I n t h r e e

- p i n p o r t s , p i n s n e a r t h e n i c k s a r e s i g n a l p i n s

.

· A f t e r c h o o s i n g a l o c a t i o n t o m o u n t t h e M C

, i t i s

· r e c o m m e n d e d t h a t y o u D O N O T m o u n t t h e M C

· u n t i l a l l w i r i n g s a n d s o f t w a r e c o n f i g u r a t i o n s a r e c o m p l e t e d

. ( O p t i o n a l ) G P S / C O M P A S S

· G P S / C o m p a s s i s s e n s i t i v e t o m a g n e t i c i n t e r f e r e n c e , s h o u l d b e f a r a w a y f r o m a n y e l e c t r o n i c d e v i c e s

.

· Y o u s h o u l d u s e e p o x y r e s i n A B g l u e t o a s s e m b l e t h e G P S b r a c k e t f i r s t a s t h e f i g u r e s h o w e d i n

p r e v i o u s p a g e

.

· M o u n t t h e b r a c k e t o n t h e c e n t e r p l a t e o f c r a f t f i r s t

, t h e n f i x t h e G P S o n t h e p l a t e o f t h e b r a c k e t ( b y 3 M g l u e p r o v i d e d )

. T h e G P S i s s e n s i t i v e t o v i b r a t i o n i n t e r f e r e n c e , s o p o s i t i o n t h e b r a c k e t a t l e a s t 1 0

c m f r o m a n y r o t o r

.

· T h e D J I l o g o m a r k e d o n t h e G P S s h o u l d f a c e t h e s k y , w i t h t h e o r i e n t a t i o n a r r o w p o i n t i n g d i r e c t l y f o r w a r d

. T h e G P S / C o m p a s s i s p a c k a g e d w i t h a s p e c i a l i n d i c a t i o n l i n e f o r m o u n t i n g f o r t h e f i r s t t i m e

.

· I f y o u a r e u n c e r t a i n w h e t h e r m a t e r i a l s n e a r t h e G P S / C o m p a s s m o d u l e a r e m a g n e t i c o r n o t

, y o u c a n

u s e a c o m p a s s o r m a g n e t t o c h e c k i t

. I f y o u u s e y o u r o w n m o u n t i n g r o d

, m a k e s u r e i t i s N O T

m a g n e t i c ! 3

- p o s i t i o n s w i t c h c h a n n e l T O B a t t e r y

I m p o r t a n t : t h e c o n t i n u o u s
o u t p u t o f t h e V U i s 3 A @ 5 V

, a n d t h e m a x i m u m i n s t a n t c u r r e n t i s 7

. 5 A

. I f t h e V U c a n n o t a f f o r d t h e w o r k i n g
c u r r e n t f o r y o u r s e r v o s , p l e a s e u s e a n i n d e p e n d e n t p o w e r s u p p l y ; o t h e r w i s e , i t m a y c a u s e t h e V U s a f e g u a r d a n d l e a d t o t h e m a i n c o n t r o l l e r r e b o o t

.



# V1 is compatible with the PMU V2 (Accessory of Naza

- M V2 )

V1 system is compatible with the PMU V2 of V2 system; please ca rry out the following connection. The other

modules connection is the same as before. Important: You are asked to upgrade your Firmware version of V1 MC to V3.10 or above, as the PUM V2 can only

work with the MC of version 3.10 or above.

t a k e p o s i t i v e p o w e r s u p p l y D i s c o n n e c t i o n T a k e n e g a t i v e p o w e r s u p p l y

### © 201 5 DJI . All Rights Reserved. 

## 27 | 

# V

1 Port Description
Please remember the function of each port, which may help you to use the N aza

- M efficiently.



# Main Controller

A For roll control (left/right)



## E For pitch control (front /back)



## T For throttle control



## R For rudder control



## U For Control Mode Switch



## X 1 For gimbal pitch control Or for gain tuning



## X 2 For D

- Bus (S

- Bus / S

- Bus 2 compatible) Or for gain tuning Or for IOC switch



## X 3 For voltage monitor (Connect with VU V

- SEN port)



## M 1 To #1 rotor



## M 2 To #2 rotor



## M 3 To #3 rotor



## M 4 To #4 rotor



## M 5 To #5 rotor



## M 6 To #6 rotor



## F 1 To gimbal roll servo Or t o # 7 rotor (Upgrade the MC Firmware to V3.10 or above)



## F 2 To gimbal pitch servo Or t o # 8 rotor (Upgrade the MC Firmware to V3.10 or above)

L E D 

## LED port, for LED wire connection from Versatile Unit

E X P

. 

## GPS port, fo r GPS module wire connection.

(In three

- pin ports, pins near the nicks are signal pins.)


# Versatile Unit

V

- SEN V

- SEN port: To the X3 port of the main controller, for monitoring battery voltage and supplying

power

z Orange wire (signal wire) output: ± 3.3V

z Red wire (power wire) output: 3 A@5V

LED LED wire, to LED port of the main controller.

USB port: PC connection for configuration and firmware upgrades. 

# Optional GPS & Compass

Connect to the EXP. port.

### © 201 5 DJI . All Rights Reserved. 

## 28 | 

# V1 Specification

General

Built

- In Functions z Three Modes of Autopilot

z Enhanced Fail Safe

z Low Voltage Protection

z S

- Bus / S

- Bus 2 Receiver Support

z PPM Receiver Support

z 2

- axle Gimbal Support 

# Peripheral

Supported Multi

- rotor z Quad

- rotor I4, X4;

z Hexa

- rotor I 6, X6, IY6, Y6.

z Octo

- rotor I 8, V 8, X 8 (Upgrade the MC Firmware to

V3.10 or above)

Supported ESC output 400Hz refresh frequency.

Recommended Transmitter PCM or 2.4GHz with a minimum 4 channels.

Assistant Software System Requirement Windows XP SP3; Windows 7


# Electri cal & Mechanical

Working Voltage Range z MC: 4.8V ~ 5.5 V

z VU Input: 7.2V ~ 26.0 V (recommend 2S ~ 6S LiPo) Output( V

- SEN port red wire ): 3A@5V Output( V

- SEN port red wire )burst current:7.5A Power Consumption z MAX: 1.5W(0.3A@5V)

z Normal: 0.6W(0.1 2A@5V)

Operating Temperature

- 10°C

~ 50°C(14F ~122F)

Weight z MC: 25g

z GPS: 21.3g

z VU: 20g

Dimensions z MC: 45.5mm × 31.5mm × 18.5mm

z GPS & Compass: 46mm (diameter) x 9mm

z VU: 32.2mm × 21.1mm × 7.7mm 

# Flight Performance (can be effected by mechanical performa nce and payloads)
Hovering Accuracy (GPS Mode) z Vertical: ± ± 0.8m

z Horizontal: ± ± 2.5m
Max Yaw Angular Velocity 200°/s

Max Tilt Angle 45°
Max Ascent / Descent Speed ±6m/s

### © 201 5 DJI . All Rights Reserved. 

## 29 | 

# FAQ

Abnormal LED Indication List
During the Checking Procedure, if abnormal LED Indicator occurs or even the system cannot work normally, please

refer to the following list and aids troubleshooting.

(1) “System initializing and self

- checking LED flashes” are not correct ( Red LED

appears in the l ast four green flashes). The autopilot system works abnormally. Please contact your

dealer.

(2) LED blinks Yellow 4 times quickly ( )

. The system is warming up. You cannot start the motors until

the 4 rapid yellow flas hes disappear. If the warm up waiting is longer than 2 minutes, please power off for

5 minutes, cold start, and then connect the assistant software, enter the "Tools"

- > IMU calibration, carry

out the Advanced calibration.

(3) After the system start and self

- checking has finished, if the LED blinks Red, Green and Yellow ( )

continually. Sensor error is too big. Please connect the assistant software, enter the "Tools"

- > IMU

calibration, carry out calibration.

(4) At the first motors sta rt, the system will check the sensors Bias and you are asked to keep the aircraft
stationary (no need of horizontal level). If you cannot start the motors and the LED blinks Green 6 times

quickly ( ), it means that the sensor error is too big. Please connect the assistant software,

enter the "Tools"

- > IMU calibration, carry out basic calibration.

Note: after the first successful motors start, this checking will be disabled and it is no need any more to

keep the ai rcraft stationary during starting motors.

(5) The system blinks Red LED quickly during flying. Low

- voltage protection is triggered. Please land the

aircraft ASAP.

(6) The system blinks Yellow LED quickly during flying. FailSafe Mode is triggered. Pay attention tha t there is

no tall buildings and trees to block your aircraft during go

- home.

(7) The LED blinks Red and Yellow alternately ( ). Compass error is too big.

a) There may be a ferromagnetic substance close to the Phantom. Li ft the aircraft up about 1m from

the ground, if there is no Red and Yellow flashing, then it will not affect the flight.

b) Otherwise, re

- calibrate the compass.

c) If re

- calibration does not work, please connect to the Assistant Software, select the “Tools” and

follow the tips to carry out the required operation.



# Fix the TBE (Toilet Bowl Effect) Problem

When flying in GPS ATTI. Mode and the compass calibration has been done correctly, should you find the aircraft
rotating (Toilet bowl effect), or drifting when hovering. P lease check the GPS module mounting orientation and then

re

- do the compass calibration. Carry out the following procedure to re

- mount the GPS module.

### © 201 5 DJI . All Rights Reserved. 

## 30 | In the following diagram (view from the top), the aircraft can appear to be rotating in both cl ockwise and

counter

- clockwise direction, please re

- mount the GPS module correspondingly.

is the rotating direction of aircraft, is the nose direction of aircraft

,
is th e arrow direction on the GPS module, θ is the offset angle for GPS re

- mounting(about 10~30 o 

## )

Clockwise rotating GPS re

- mounting Counter Clockwise rotating GPS re

- mounting



## θ θ



# Sh ould you find the multi

- rotor does not track straight in forward flight

. Please carry out several more courses, the system will fix it automatically.



# Motors Start failure caused by TX stick(s) mid

- point error too big
If the TX stick(s) mid

- point error is too big, Motors Start will fail when you execute the Combination Stick

Commands (CSC) and lead to the aircraft will not takeoff.. And the LED will blink Red four times per second

continually to warn you.

TX stick(s) mid

- point error too big can be caused by the following reasons:

(1) There is TX stick (except the throttle stick) not at center when power on the autopilot system

. (2) The TX sticks has been trimmed, which lead s to the large deviation of mid

- point . For example, the

SUB

- TRIM has been adjusted for Futaba transmitter.

(3) The TX stick(s) travel has larger asymmetry.
For the reason (1), please put all TX sticks at the mid

- point , and then power cycle the autopilot system to re

- record

the mid

- point . If the problem continues, that can be caused by the reason (2) or reason (3), yo u need to adjust the

output range of your TX, and then use the Assistant S oftware to redo the TX calibration. Please carry out the

following procedures.

(1) Connect to the Assistant software, click Basic

- > R/C

- > Command Sticks Calibration, and p ush all TX

sticks throughout their complete travel range to see if any stick cannot reach its largest position.

(2) Adjust the largest travel of TX stick until the cursor on the Assistant software can reach both end

positions, according to your TX manual.

(3) Powe r cycle the autopilot system, note that power cycle is required.

(4) Redo the TX calibration according to the Assistant software.

### © 201 5 DJI . All Rights Reserved. 

## 31 | 

# Attitude C ontrol lable When One Motor Output is Failed

F or Hexa

- rotor, including Hexa

- rotor I, Hexa

- rotor V, Hexa

- rotor IY and Hexa

- rotor Y, aircraft is attitude controllable

when one motor output is failed.

T he NAZA

- M can still control the attitude of the Hexa

- rotor for a s afe landing when one motor output of the

Hexa

- rotor has failed, for example, one motor is st opped or one propell er is broken, etc.

T he control mode of NAZA

- M should be in Atti. Mode or GPS Atti. Mode . T he aircraft will rotate, due to an

imbalance of torque; however, it can still be controlled by the Transmitter

.
Select Course lock or home lock mode for flying the ai rcraft into a safe area to land when the aircraft is far away or

the attitude can ’ t be recognized. Even when the multi rotor is rotating, using Course lock or home lock mode will

allow you to move the mul ti rotor in the corresponding T ransmitter stick dire ction

. 

# When used with other DJI products

The NAZA

- M system communicates with other DJI products (e.g

. H3

- 2D gimbal, BTU module, iOSD mini and iOSD

Mark II) via the CAN

- Bus port ( ) of the NAZA PMU V2. You can p lug new DJI produc ts into any spare CAN

- Bus

port , since CAN

- Bus port s on NAZA

- M, CAN HUB , GCU, iOSD mini, iOSD Mark II and 2.4G Bluetooth Datalink are

the same for the communication s

. When there are not enough CAN

- Bus ports for additional DJI products, then a DJI CAN HUB mo dule is

recommended. The following diagram is for your connection reference.

Fig.1 Used with iOSD M ark II

### © 201 5 DJI . All Rights Reserved. 

## 32 | Fig. 2 Used with CAN HUB

Fig.3 Use a CAN HUB to connect the 2 .4G Bluetooth Datalink

U sers can use the NM Assistant on the mobile device when a BTU module is connecting with the Ground end of the2.4G Bluetooth Datalink (No need to connect another BTU module to the Flight

control system)

.