使用si万博1manbetxmulink®基于Parrot®系列的迷你式无人机来对四轮驱动器进行建模。为了管理模型和源文件，它使用项目管理。

“从事Lunar模块数字自动驾驶仪的设计是我作为工程师职业的亮点。当尼尔·阿姆斯特朗（Neil Armstrong）离开LM（月球模块）到月球表面时，每位为阿波罗计划做出贡献的工程师都感到骄傲感和成就。我们已经成功实现了我们的目标。我们开发了以前从未存在过的技术，并且通过努力工作和对细节的细致关注，我们创造了一个完美无缺的系统。”- Richard J. Gran，Apollo 11 Moon Landing：当时和现在的航天器设计

这个项目显示了如何模型美国宇航局HL-20 lifting body with Simulink®, Stateflow® and Aerospace Blockset™ software. The vehicle model includes the aerodynamics, control logic, fault management systems (FDIR), and engine controls (FADEC). It also includes effects of the environment, such as wind profiles for the landing phase. The entire model simulates approach and landing flight phases using an auto-landing controller. To analyze the effects of actuator failures and wind gust variation on the stability of the vehicle, use the "Run Failure Analysis in Parallel" project shortcut. If Parallel Computing Toolbox™ is installed, the analysis is run in parallel. If Parallel Computing Toolbox™ is not installed, the analysis is run in serial. Visualization for this model is done via an interface to FlightGear, an open source flight simulator package. If the FlightGear interface is unavailable, you can simulate the model by closing the loop using the alternative data sources provided in the Variant block. In this block, you can choose a previously saved data file, a Signal Editor block, or a set of constant values. This example requires Control System Toolbox™.

How to use MathWorks® products to address the technical and process challenges of aircraft design using the design of a lightweight aircraft.

如何使用理想的空速校正块来计算来自真实空速的指示空速。Aerospace Blabsset™块以红色表示。

如何使用理想的空速校正块从指示的空速中计算真实的空速。Aerospace Blabsset™块以红色表示。