Figure 1 - uploaded by Marcello Sparasci
Content may be subject to copyright.
Download
View publication
1: Ingenuity 3D model

1: Ingenuity 3D model

Source publication
Figure 1.1: Ingenuity 3D model
Figure 1.3: The CLF5605 airfoil cross section at 3/4-span
Figure 1.5: Mars Helicopter Landing gear system
Figure 1.6: Landing gear deployment hinge and flexure/damper mechanism
+22 Figure 1.8: NASA technician is shown working on Ingenuity that features...
Nonlinear modeling and control of coaxial rotor UAVs with application to the Mars helicopter
Thesis
Full-text available
  • Dec 2022
The Red Planet has been on top in the priority list of interplanetary exploration of the solar system. The Mars exploration landers and rovers have laid the foundation of our understanding of the planet atmosphere and terrain. Although the rovers have been a great help, they also have limitations in terms of their speed and exploration capabilities...
Cite
Download full-text

Citations

... In the next sections, we will study and examine the equations as well as their control structures. For further information on these equations, you can refer to references [41][42][43][44][45]. ...
Analytical Design of Optimal Model Predictive Control and Its Application in Small-Scale Helicopters
Article
Full-text available
  • Apr 2023
A new method for controlling the position and speed of a small-scale helicopter based on optimal model predictive control is presented in this paper. In the proposed method, the homotopy perturbation technique is used to analytically solve the optimization problem and, as a result, to find the control signal. To assess the proposed method, a small-scale helicopter system is modeled and controlled using the proposed method. The proposed method has been investigated under different conditions and its results have been compared with the conventional predictive control method. The simulation results show that the proposed technique is highly proficient in the face of various uncertainties and disturbances, and can quickly return the helicopter to its path.
View
View