model-based simulink design environment Search Results


amesim–simulink co-simulation model  (MathWorks Inc)
95
MathWorks Inc amesim–simulink co-simulation model
Amesim–Simulink Co Simulation Model, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 95/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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simulink model  (MathWorks Inc)
90
MathWorks Inc simulink model
Simulink Model, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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simulink model - by Bioz Stars, 2026-03
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matlab/simulink  (MathWorks Inc)
90
MathWorks Inc matlab/simulink
Matlab/Simulink, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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timer-based simulink model  (MathWorks Inc)
90
MathWorks Inc timer-based simulink model
Timer Based Simulink Model, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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matlab-simulink  (MathWorks Inc)
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MathWorks Inc matlab-simulink
Matlab Simulink, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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hybrid powertrain model  (MathWorks Inc)
94
MathWorks Inc hybrid powertrain model
Hybrid Powertrain Model, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 94/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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simulink-based moma experiment simulator (momasim) model  (MathWorks Inc)
90
MathWorks Inc simulink-based moma experiment simulator (momasim) model
The design of <t>MOMA</t> instrument. The CAD model (left) and the flight model instrument (top right). A picture of the linear ion trap (LIT) is also shown here (down right).
Simulink Based Moma Experiment Simulator (Momasim) Model, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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models of all simulink-based drivers  (MathWorks Inc)
90
MathWorks Inc models of all simulink-based drivers
The design of <t>MOMA</t> instrument. The CAD model (left) and the flight model instrument (top right). A picture of the linear ion trap (LIT) is also shown here (down right).
Models Of All Simulink Based Drivers, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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loop frommatlab simulink  (MathWorks Inc)
96
MathWorks Inc loop frommatlab simulink
The design of <t>MOMA</t> instrument. The CAD model (left) and the flight model instrument (top right). A picture of the linear ion trap (LIT) is also shown here (down right).
Loop Frommatlab Simulink, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 96/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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simulink® model  (MathWorks Inc)
90
MathWorks Inc simulink® model
The design of <t>MOMA</t> instrument. The CAD model (left) and the flight model instrument (top right). A picture of the linear ion trap (LIT) is also shown here (down right).
Simulink® Model, supplied by MathWorks Inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
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Image Search Results


The design of MOMA instrument. The CAD model (left) and the flight model instrument (top right). A picture of the linear ion trap (LIT) is also shown here (down right).

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: The design of MOMA instrument. The CAD model (left) and the flight model instrument (top right). A picture of the linear ion trap (LIT) is also shown here (down right).

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques:

The operation of the MOMA instrument in LDI-MS mode. The time (x-axis) is not to scale.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: The operation of the MOMA instrument in LDI-MS mode. The time (x-axis) is not to scale.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques:

Optimized set of operational parameters of MOMA MS.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: Optimized set of operational parameters of MOMA MS.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques:

The overall electrode configuration and key dimensions of the linear ion trap on MOMA.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: The overall electrode configuration and key dimensions of the linear ion trap on MOMA.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques:

(A) 3D model of the cross-section of MOMA aperture valve. In this depiction, “a” indicates the vacuum side ion inlet tube with a length of 1.5 cm: “b” points to the continuation of the ion inlet tube embedded within the slide, with a tube length of 0.5 cm; and “c” shows the air-side (or Mars-side) ion inlet tube facing the sample, with a tube length of 1 cm. (B) Engineering Test Unit (ETU), or pre-flight version, of the aperture valve mounted on mockup of the interface to the mass spectrometer’s mechanical housing. (C) A recorded pressure pulse on the flight system is shown for a valve opening time of 100 ms, with Mars pressure held at 0.8 kPa (or 6 Torr) and the mass spectrometer chamber actively pumped.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: (A) 3D model of the cross-section of MOMA aperture valve. In this depiction, “a” indicates the vacuum side ion inlet tube with a length of 1.5 cm: “b” points to the continuation of the ion inlet tube embedded within the slide, with a tube length of 0.5 cm; and “c” shows the air-side (or Mars-side) ion inlet tube facing the sample, with a tube length of 1 cm. (B) Engineering Test Unit (ETU), or pre-flight version, of the aperture valve mounted on mockup of the interface to the mass spectrometer’s mechanical housing. (C) A recorded pressure pulse on the flight system is shown for a valve opening time of 100 ms, with Mars pressure held at 0.8 kPa (or 6 Torr) and the mass spectrometer chamber actively pumped.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques: Mass Spectrometry

Performance requirements for the MOMA pressure sensor in LDI-MS mode of operation (dynamic pressure environment). The required sensor accuracy over various ranges was chosen to meet experiment and instrument operating requirements (specifically at the relatively fast response time) under the full range of mission operating conditions. They are not reflective of the ultimate performance of the sensor if fully characterized and calibrated. The required sensor response time is 0.25 s, which was chosen to match with the typical pump down time, from 50 mtorr to 0.1 mtorr, of 0.6–0.9 s.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: Performance requirements for the MOMA pressure sensor in LDI-MS mode of operation (dynamic pressure environment). The required sensor accuracy over various ranges was chosen to meet experiment and instrument operating requirements (specifically at the relatively fast response time) under the full range of mission operating conditions. They are not reflective of the ultimate performance of the sensor if fully characterized and calibrated. The required sensor response time is 0.25 s, which was chosen to match with the typical pump down time, from 50 mtorr to 0.1 mtorr, of 0.6–0.9 s.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques:

Dynamic response of the MOMA-MS MEMS Pirani sensor (red solid line) upon actuation of the pulsed solenoid valve is compared with the capacitive pressure sensor (Baratron) measurement (black dashed line) under flight-like pumping and electronic noise conditions. Inset: (Top left) Photos of the MEMS Pirani sensor with and without the lid of the T039 package. (Top right) Photo of the sensor without the silicon microbridge [31] with Rp, Rk. and connections to the MEMS Pirani control circuit in the flight electronics schematically indicated.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: Dynamic response of the MOMA-MS MEMS Pirani sensor (red solid line) upon actuation of the pulsed solenoid valve is compared with the capacitive pressure sensor (Baratron) measurement (black dashed line) under flight-like pumping and electronic noise conditions. Inset: (Top left) Photos of the MEMS Pirani sensor with and without the lid of the T039 package. (Top right) Photo of the sensor without the silicon microbridge [31] with Rp, Rk. and connections to the MEMS Pirani control circuit in the flight electronics schematically indicated.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques: Control

(a) LDI-MS spectrum acquired on the MOMA flight mass spectrometer for single-crystal CSI to demonstrate performance requirements for mass range, resolution and accuracy. (b) LDI-MS spectrum acquired on the MOMA ETU for 50 fmol/mm2 R6G demonstrates high sensitivity for conjugated organics.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: (a) LDI-MS spectrum acquired on the MOMA flight mass spectrometer for single-crystal CSI to demonstrate performance requirements for mass range, resolution and accuracy. (b) LDI-MS spectrum acquired on the MOMA ETU for 50 fmol/mm2 R6G demonstrates high sensitivity for conjugated organics.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques: Mass Spectrometry

(A) LDI-MS spectra acquired on the MOMA brassboard ion trap instrument of coronene doped nontronite. (B) isolation of m/z 225–700 Da and (C) enhancement of the analyte signal with increased laser shots.

Journal: International journal of mass spectrometry

Article Title: Mars Organic Molecule Analyzer (MOMA) laser desorption/ionization source design and performance characterization

doi: 10.1016/j.ijms.2017.03.010

Figure Lengend Snippet: (A) LDI-MS spectra acquired on the MOMA brassboard ion trap instrument of coronene doped nontronite. (B) isolation of m/z 225–700 Da and (C) enhancement of the analyte signal with increased laser shots.

Article Snippet: Initial selection of suitable tube dimensions was made based on the Simulink-based MOMA experiment SIMulator (MOMASIM) model of the vacuum system, anticipated pressure load, and targeted pump down time.

Techniques: Isolation