AeroSpace Simulation : AeroSpace-SIM v1.0 (Missile + Flight + LEO + Performance/Stability Chart) Part. 4

  Previous Work Status

Initial Version of Missile-SIM for Performance evaluation
Aerodynamic Validation of Missile-SIM for Trajectory 
AIM-120C Study using Missile-SIM : Part 1 - Sensitivity
AIM-120C Study using Missile-SIM : Part 2 - Launch Condition
AIM-120C Study using Missile-SIM : Part 2 - Launch Condition - revision
Patch note of Missile-SIM : Guidance Algorithm is added w/ Real-Time plot
W.I.P status of Missile-SIM : Addition of Air-propulsion part 1
W.I.P status of Missile-SIM : Addition of Air-propulsion part 2
AIM-120C Study using Missile-SIM : Part 3 - CUDA / LREW / METEOR types. 1 : Baseline Comparison
AIM-120C Study using Missile-SIM : Part 3 - CUDA / LREW / METEOR types. 2 : Sensitivity Analysis
AIM-120C Study using Missile-SIM : Part 3 - CUDA / LREW / METEOR types. 3 : Few mentions

Meteor as New Anti-Radar missile for SEAD?

Missile-SIM : Performance Evaluation for Iskander / Kh-47M2 Kinzhal & ATACMS+Booster

Flight-SIM : Trajectory & Performance Analysis for Jet Aircraft

Flight-SIM : DB Structure of the SIM

Flight-SIM : W.I.P of the SIM

Flight-SIM : Generic DB of single-aisle Airliner : Part 1 

Flight-SIM : Generic DB of single-aisle Airliner : Part 2

Flight-SIM : W.I.P of the SIM II

Flight-SIM : Initial Version of the Flight-SIM w/ Demo

The new topic for My page : Optimization of Supersonic aerodynamic aircraft

Supersonic Airliner design using Joint wing (Diamond wing) - Part 1

Supersonic Airliner design using Joint wing (Diamond wing) - Part 2

AeroSpace Simulation : AeroSpace-SIM v1.0 (Missile + Flight + LEO + Performance/Stability Chart) Part. 1

AeroSpace Simulation : AeroSpace-SIM v1.0 (Missile + Flight + LEO + Performance/Stability Chart) Part. 2

AeroSpace Simulation : AeroSpace-SIM v1.0 (Missile + Flight + LEO + Performance/Stability Chart) Part. 3

AerospaceSIM - GitLab

 4. Demo-Case Result

8) Performance Chart

Ps, Fuel Flow, Specific Range (V/FF = m/s / kg/s = m/kg), Turn rate is described for the generic airliner DB. Due to the low resolution of sim, graph is very rough, but functioning of the program is checked. 

9) Stability Chart

State Space maxtrix A, B and its eigen value is calculated by the SIM. Below shows test result for A matrix for longitudinal and lateral direction. Based on matrix value, exact controller design should be done in MATLAB or similar framework. 

The End