衛星與火箭導航技術：從慣性到量子感測

Navigation Technologies for Satellites and Launch Vehicles：From Inertial to Quantum Sensing

學期

114-2

學分

3 學分

當期課號

536076

永久課號

ENSS30022

開課單位

太空系統工程研究所、機械工程學系

授課教師

張存均

校區

光復

類別

選修

上課時間表

節	週二
2 09:00–09:50	衛星與火箭導航技術：從慣性到量子感測 EE206（光復） 3 節連堂
3 10:10–11:00
4 11:10–12:00

* 根據陽明交大上課時間表所列

概述

This course focuses on navigation and sensing technologies for aerospace vehicles such as satellites and launch vehicles. It provides a systematic introduction ranging from conventional inertial navigation systems (INS), global navigation satellite systems (GNSS), and multi-sensor integration, to emerging quantum sensing and quantum navigation approaches. Students will examine the challenges of navigation during ascent, orbital, and reentry phases, and explore how quantum technologies can offer future solutions for interference-resilient, high-precision, and long-duration navigation. By the end of the semester, students are expected to be able to: 1. Develop a comprehensive understanding of aerospace navigation and sensing systems. 2. Model and analyze inertial and GNSS-integrated navigation for satellite and rocket missions. 3. Acquire core knowledge of multi-sensor fusion and guidance laws for launch vehicles. 4. Gain familiarity with quantum sensing technologies (cold-atom interferometers, NV centers) and their aerospace applications. 5. Build the ability to evaluate and compare conventional and quantum navigation approaches. 6. Strengthen innovative thinking in designing alternative navigation architectures for GNSS-denied environments.

先修科目

General Physics, Calculus, and Engineering Mathematics

備註

無備註

教學方式

All of the course materials will be available on e3, including lecture notes and homework solutions. Teaching Assistants: TBD

評分方式

Class participation (in-class exercises, quizzes, and homework): 20% Midterm Exam: 40% Final Exam: 40%

課程大綱

教師未提供此項資料

週次計畫

週次	主題
第 1 週	Course overview: evolution of aerospace navigation and sensing; mission requirements and challenges
第 2 週	Introduction to aerospace navigation: conventional systems in satellite and rocket missions
第 3 週	Basics of inertial navigation systems (INS): accelerometers, gyroscopes, strapdown algorithms
第 4 週	INS error sources, drift mechanisms, compensation methods; application examples
第 5 週	Fundamentals of GNSS and multi-constellation systems
第 6 週	GNSS/INS integration; Kalman filtering; sensor fusion with star trackers and magnetometers
第 7 週	Rocket navigation and guidance laws: PN, ZEM; ascent and reentry challenges
第 8 週	Midterm Exam
第 9 週	Introduction to quantum navigation: coherence, interference, categories of quantum sensors
第 10 週	Cold-atom interferometers: principles, accelerometers, and gyroscopes
第 11 週	On-orbit cold-atom experiments and applications in aerospace missions
第 12 週	NV centers in diamond: physics and magnetometry
第 13 週	NV-based nuclear-spin gyroscopes: principles, challenges, aerospace feasibility
第 14 週	Comparative analysis: conventional vs. quantum navigation (FOG, RLG, MEMS vs. cold-atom, NV)
第 15 週	International programs (DARPA, ESA, CNSA); GNSS-denied navigation alternatives
第 16 週	Final Exam

教科書

No specific textbook is appointed, but you may refer to the references below: "Modern Spacecraft Guidance, Navigation, and Control: From System Modeling to AI and Innovative Applications" by Vincenzo Pesce, Andrea Colagrossi, Stefano Silvestrini, Elsevier, 2023. "Global Navigation Satellite Systems, Inertial Navigation, and Integration (4th Edition)" by Mohinder S. Grewal, Angus P. Andrews, Chris Bartone, Wiley, 2020. "Spacecraft Dynamics and Control: A Practical Engineering Approach" by Sidi, Marcel J, Cambridge University Press, 2020. "Introduction to Quantum Science and Technology" by David S. Simon, Springer, 2025. "Quantum Communication, Quantum Networks, and Quantum Sensing" by Ivan B Djordjevic, Academic Press, 2022.

Office Hours

地點: EE421
時間: By appointment
聯絡方式: Ext: 55131 Email: changtc@nycu.edu.tw