Strategic Objectives
• Master the integration of miniaturized reaction wheels for agile maneuvering.
• Understand the algorithmic logic behind star tracker celestial navigation.
• Leverage magnetorquers to harness Earth's magnetic field for desaturation.
• Design control loops tailored specifically for low-moment-of-inertia frames.
The Core Challenge
Small-scale satellites face unique physics challenges where traditional ADCS solutions are too bulky or power-hungry to survive.
01
Foundations of Spacecraft Orientation
02
The Physics of Rotation
03
Kinematic Representations
04
Sensory Perception
05
Stellar Navigation
06
Magnetic Field Awareness
07
Solar Aspect Sensing
08
Rate Sensing and Gyroscopes
09
The Momentum Exchange
10
Magnetic Torque Generation
11
Momentum Management
12
Control Loop Theory
13
The Kalman Filter
14
Disturbance Torques
15
Small-Sat Dynamics
16
The CubeSat Revolution
17
On-Board Processing
18
Active Magnetic Control
19
Ground Testing and Simulation
20
Orbital Perturbations
21