QJ 3289-2007 Hardware-in-the-Loop Simulation Requirement and Method for Control System of Ground-to-Air Radio Frequency Homing Missiles (English Version)
Hardware-in-the-loop simulation requirement and method for control system of ground-to-air radio frequency homing missiles
1 Scope
This standard specifies the hardware-in-the-loop simulation requirement and method for control system of ground-to-air radio frequency homing missiles.
This standard is applicable to the hardware-in-the-loop simulation test for control system of ground-to-air radio frequency homing missiles.
2 Normative references
The following normative documents contain provisions which, through reference in this standard, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions, of any of these publications do not apply to this standard. However, parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the latest edition applies.
QJ 2281-1992 Specification for hardware-in-the-loop simulation test of ground-to-air (ship-to-air) missiles
3 Terms and definitions
For the purposes of this standard, the following terms and definitions apply.
3.1
simulation model
equivalent model transformed from a mathematical model in a certain way, which can run on a computer
3.2
real-time simulation
simulation of which the time history is equal to and one-to-one corresponds to that of the real system
3.3
hardware-in-the-loop simulation
real-time simulation with at least one missile control system hardware connected in the missile guidance and control loop
3.4
hardware employed simulation
missile control system hardware which is connected to the simulation system and participates in the hardware-in-the-loop simulation test
3.5
radio frequency homing
process of obtaining guidance information by using the radio frequency (RF) seeker to receive the target-radiated or -reflected energy
4 Test requirements
4.1 Simulation test objective
The simulation test is carried out to inspect and verify the correctness of the design of control system of ground-to-air radio frequency homing missiles, so as to improve and optimize the model design.
4.2 Test principles and requirements for missile guidance and control equipment hardware
Foreword i 1 Scope 2 Normative references 3 Terms and definitions 4 Test requirements 5 Test methods
QJ 3289-2007 Hardware-in-the-Loop Simulation Requirement and Method for Control System of Ground-to-Air Radio Frequency Homing Missiles (English Version)
Standard No.
QJ 3289-2007
Status
valid
Language
English
File Format
PDF
Word Count
8500 words
Price(USD)
255.0
Implemented on
2007-11-1
Delivery
via email in 1 business day
Detail of QJ 3289-2007
Standard No.
QJ 3289-2007
English Name
Hardware-in-the-Loop Simulation Requirement and Method for Control System of Ground-to-Air Radio Frequency Homing Missiles
Hardware-in-the-loop simulation requirement and method for control system of ground-to-air radio frequency homing missiles
1 Scope
This standard specifies the hardware-in-the-loop simulation requirement and method for control system of ground-to-air radio frequency homing missiles.
This standard is applicable to the hardware-in-the-loop simulation test for control system of ground-to-air radio frequency homing missiles.
2 Normative references
The following normative documents contain provisions which, through reference in this standard, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions, of any of these publications do not apply to this standard. However, parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the latest edition applies.
QJ 2281-1992 Specification for hardware-in-the-loop simulation test of ground-to-air (ship-to-air) missiles
3 Terms and definitions
For the purposes of this standard, the following terms and definitions apply.
3.1
simulation model
equivalent model transformed from a mathematical model in a certain way, which can run on a computer
3.2
real-time simulation
simulation of which the time history is equal to and one-to-one corresponds to that of the real system
3.3
hardware-in-the-loop simulation
real-time simulation with at least one missile control system hardware connected in the missile guidance and control loop
3.4
hardware employed simulation
missile control system hardware which is connected to the simulation system and participates in the hardware-in-the-loop simulation test
3.5
radio frequency homing
process of obtaining guidance information by using the radio frequency (RF) seeker to receive the target-radiated or -reflected energy
4 Test requirements
4.1 Simulation test objective
The simulation test is carried out to inspect and verify the correctness of the design of control system of ground-to-air radio frequency homing missiles, so as to improve and optimize the model design.
4.2 Test principles and requirements for missile guidance and control equipment hardware
Contents of QJ 3289-2007
Foreword i
1 Scope
2 Normative references
3 Terms and definitions
4 Test requirements
5 Test methods
