Dr. Shane Ross
Dr. Shane Ross
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Trajectories with Prescribed Itineraries and MATLAB Tutorial, 3-Body Problem Topic 15
To find trajectories with prescribed itineraries, numerical methods are needed, namely for generating periodic orbits and their invariant manifolds. We outline an algorithm for using these methods to generate a trajectory with a prescribed itinerary in the planar CR3BP. An example computation in MATLAB is given for taking a Poincare section of a stable manifold tube on a Lagrangian L1 Lyapunov orbit.
💻 *MATLAB Code* Live Code File Format (.mlx).
⬇️ *Download* at tinyurl.com/cr3bpmatlab
*Look for:* cr3bp_tube_manifolds.mlx
Execute the file in MATLAB
▶️ Previous: 3-Body Problem Periodic Orbits & Stable Manifolds using Differential Correction, MATLAB | Topic 14
czcams.com/video/cwRFd7GcE58/video.html
▶️ *Three-Body Problem Introduction*
czcams.com/video/ZE299fDuPjc/video.html
▶️ *Related: Applications to Dynamical Astronomy*
czcams.com/video/fV0kUmtQWZU/video.html
► Reference: Chapter 4, "Construction of Trajectories with Prescribed Itineraries"
of the PDF book:
*Dynamical Systems, the Three-Body Problem and Space Mission Design*
Koon, Lo, Marsden, Ross (2022)
*Download for free* at shaneross.com/books
► *PDF Lecture Notes (Lecture 11 for this video)*
is.gd/3BodyNotes
The circular restricted 3-body problem (CR3BP) describes the motion of a body moving in the gravitational field of two primaries that are orbiting in a circle about their common center of mass, with trajectories such as Lagrange points, halo orbits, Lyapunov planar orbits, quasi-periodic orbits, quasi-halos, low-energy trajectories, etc.
• The two primaries could be the Earth and Moon, the Sun and Earth, the Sun and Jupiter, etc.
• The mass parameter μ = m2/(m1 + m2) is the main factor determining the type of motion possible for the spacecraft. It is analogous to the Reynold's number Re in fluid mechanics, determining the onset of new types of behavior.
► Dr. Shane Ross is an Aerospace Engineering Professor at Virginia Tech. He has a Caltech PhD, worked at NASA/JPL and Boeing on interplanetary trajectories, and is a world renowned expert in the 3-body problem. He has written a book on the subject (link above).
► Follow me
RossDynamicsLab
► *CHAPTERS*
0:00 Introduction, Summary
2:35 Find region with desired itinerary for trajectory
6:33 Step 1, Select appropriate energy
7:59 Step 2, Compute Lagrange point eigenvalues & eigenvectors
8:40 Step 3, Compute Lyapunov orbits via numerical continuation
13:39 MATLAB tutorial begins, code provided (see link above)
17:55 Step 4, Compute stable and unstable invariant manifold tubes
23:13 Step 5, Poincare section of tube
29:04 Step 6, Compute other tube Poincare sections
31:52 Step 7, Pick initial condition in intersection of tubes (X,J,S)
34:26 Tube intersection after several circuits about secondary mass
38:15 Temporarily captured satellite of Jupiter
38:22 Longer itinerary construction (X,J,S,J,X)
► *Courses & Playlists by Dr. Ross*
▶️ 3-Body Problem Orbital Dynamics
is.gd/3BodyProblem
▶️ Space Manifolds
is.gd/SpaceManifolds
▶️ Space Vehicle Dynamics
is.gd/SpaceVehicleDynamics
▶️ Lagrangian & 3D Rigid Body Dynamics
is.gd/AnalyticalDynamics
▶️ Nonlinear Dynamics & Chaos
is.gd/NonlinearDynamics
▶️ Hamiltonian Dynamics
is.gd/AdvancedDynamics
▶️ Center Manifolds, Normal Forms, & Bifurcations
is.gd/CenterManifolds
symbolic dynamics Lagrange points space manifolds differential correction single and multiple shooting collocation state transition matrix variational equations tube dynamics
#orbitalmechanics #threebodyproblem #tubedynamics #manifold #periodicorbit #smalehorseshoe #symbolicdynamics #heteroclinic #homoclinic #LagrangePoint #space #CR3BP #3body #3bodyproblem #SpaceManifolds #JamesWebb #NonlinearDynamics #gravity #SpaceTravel #SpaceManifold #DynamicalSystems #solarSystem #NASA #dynamics #celestial #SpaceSuperhighway #InterplanetarySuperhighway #spaceHighway #gravitational #mathematics #dynamicalAstronomy #astronomy #wormhole #physics #chaos #unstable #PeriodicOrbits #HaloOrbit #LibrationPoint #LagrangianPoint #LowEnergy #VirginiaTech #Caltech #JPL #LyapunovOrbit #CelestialMechanics #HamiltonianDynamics #planets #moons #multibody #GatewayStation #LunarGateway #L1gateway #cislunar #cislunarspace #orbitalDynamics #orbitalMechanics #Chaotician #Boeing #JetPropulsionLab #Centaurs #Asteroids #Comets #TrojanAsteroid #Jupiter #JupiterFamily #JupiterFamilyComets #Hildas #quasiHildas #KuiperBelt
zhlédnutí: 1 674

Video

Orbital Motion in Cislunar Space
zhlédnutí 2KPřed 9 měsíci
Orbital dynamics beyond GEO is best described by a restricted 3-body model, where a spacecraft, asteroid, or piece of debris is affected by both the Earth and Moon simultaneously. We tell you the basics here. The orbital dynamics in this regime (xGEO or cislunar space), encompassing secular, resonant, chaotic, close-encounter, and manifold dynamics, is dramatically different than the weakly per...
3-Body Problem Periodic Orbits & Stable Manifolds using Differential Correction, MATLAB | Topic 14
zhlédnutí 1,9KPřed 9 měsíci
To generate the invariant stable or unstable manifold of a periodic orbit, one first needs to compute the periodic orbit as accurately as possible. To do this, one can use method of differential correction, which incorporates analytical approximations as the first guess in an iterative process aimed at producing initial conditions belonging to a periodic orbit. We give an overview of differenti...
Global Orbit Structure in the 3-Body Problem: Theorem and Examples | Topic 13
zhlédnutí 1,1KPřed 10 měsíci
Write any sequence of letters representing the whereabouts of a spacecraft, and there exists a trajectory whose itinerary follows that sequence in the restricted 3-body problem, for example, a spacecraft in the gravity fields of the Earth and Moon. This is another lecture in a series on the gravitational 3-body problem: 📚 *3-Body Problem Orbital Dynamics Course* czcams.com/play/PLUeHTafWecAXDF9...
Motion Near L4, L5 Lagrange Points- Tadpole, Horseshoe Orbit, Trojan Asteroids,Lucy Mission,Topic 12
zhlédnutí 1,2KPřed rokem
Motion around L4 and L5, the stable triangular Lagrange points or equilateral points. This is another lecture in a series on the gravitational 3-body problem: 📚 *3-Body Problem Orbital Dynamics Course* czcams.com/play/PLUeHTafWecAXDF9vWi7PuE2ZQQ2hXyYt_.html ▶️ Next: Global Orbit Structure in 3-Body Problem: Theorem and Examples, Topic 13 czcams.com/video/gLY0vqmb2D4/video.html ▶️ Previous: Traj...
Kalman Filter for Beginners, Part 3- Attitude Estimation, Gyro, Accelerometer, Velocity MATLAB Demo
zhlédnutí 17KPřed rokem
Attitude estimation from Kalman filter using sensor fusion via data from a gyroscope and accelerometer, providing angular velocity and a reference direction (direction of gravity), respectively. In the third of my three-part series, we first go over a MATLAB example of estimating position and velocity from noisy position data (altitude from sonar). We compare the estimated velocity with that fr...
Kalman Filter for Beginners, Part 2 - Estimation and Prediction Process & MATLAB Example
zhlédnutí 22KPřed rokem
Use the Kalman Filter, even without knowing all the theory! In Part 2 of my three-part series, I discuss the prediction and estimation processes, making an analogy with low-pass filters. We construct a system model via the state transition matrix A, the state-to-measurement matrix H, and the process noise and measurement noise matrices, Q and R. 💻 Get the MATLAB Code: tinyurl.com/kalmanfilterfo...
Kalman Filter for Beginners, Part 1 - Recursive Filters & MATLAB Examples
zhlédnutí 53KPřed rokem
You can use the powerful Kalman Filter, even if you don't know all the theory! Join me for Part 1 of my three-part series, where I introduce the concepts, breaking it down for you. I take a simple approach, starting with recursive filters like the average, moving average, and low-pass filters. I'll even show you real-world MATLAB examples to bring it all to life. Enhance your estimation and dat...
Trajectory Types Near L1, L2, & L3 in the Three Body Problem - Theory and MATLAB Examples | Topic 11
zhlédnutí 1,3KPřed rokem
Trajectory Types Near L1, L2, & L3 in the Three Body Problem - Theory and MATLAB Examples | Topic 11
Geometry of Motion near L1, L2, 3-Body Dynamical Systems Analysis, McGehee Representation | Topic 10
zhlédnutí 1,7KPřed rokem
Geometry of Motion near L1, L2, 3-Body Dynamical Systems Analysis, McGehee Representation | Topic 10
Physics of Gliding Animals and Plants: Insights from Models, Experiments and Bio-inspired Designs
zhlédnutí 1,2KPřed rokem
Physics of Gliding Animals and Plants: Insights from Models, Experiments and Bio-inspired Designs
Drone-Based Wind Measurements in Aquatic Environments
zhlédnutí 317Před rokem
Drone-Based Wind Measurements in Aquatic Environments
Cislunar Space: 3-Body Model of Orbital Dynamics Beyond the Geosynchronous Belt (xGEO)
zhlédnutí 2,1KPřed rokem
Cislunar Space: 3-Body Model of Orbital Dynamics Beyond the Geosynchronous Belt (xGEO)
Defunct Apollo Spacecraft Cycling Between Orbits Around Earth and Sun #shorts
zhlédnutí 1,2KPřed rokem
Defunct Apollo Spacecraft Cycling Between Orbits Around Earth and Sun #shorts
Motion Near L1 and L2: Linearized Equations of Motion in the 3-Body Problem | Topic 9
zhlédnutí 2KPřed rokem
Motion Near L1 and L2: Linearized Equations of Motion in the 3-Body Problem | Topic 9
Earth to Venus Trajectory Using NO Propulsion - Matt Werner Thesis Defense
zhlédnutí 1,5KPřed rokem
Earth to Venus Trajectory Using NO Propulsion - Matt Werner Thesis Defense
Transition Tube in Phase Space #shorts
zhlédnutí 378Před 2 lety
Transition Tube in Phase Space #shorts
Calculating Collinear Lagrange Point Positions: L1, L2, L3 in Restricted 3-Body Problem | Topic 8
zhlédnutí 2,5KPřed 2 lety
Calculating Collinear Lagrange Point Positions: L1, L2, L3 in Restricted 3-Body Problem | Topic 8
Lagrange Points L4, L5 in 3-Body Problem: Derivation of Equilateral Point Location | Topic 7
zhlédnutí 3,4KPřed 2 lety
Lagrange Points L4, L5 in 3-Body Problem: Derivation of Equilateral Point Location | Topic 7
3-Body Problem Jacobi Constant, Zero Velocity Curves, Hill Regions of Possible Motion | Topic 6
zhlédnutí 2,9KPřed 2 lety
3-Body Problem Jacobi Constant, Zero Velocity Curves, Hill Regions of Possible Motion | Topic 6
Fluid Dynamics on a Möbius Strip #shorts
zhlédnutí 622Před 2 lety
Fluid Dynamics on a Möbius Strip #shorts
3 Body Problem Hamilton's Equations -&- Why View Motion in a Rotating Frame? | Topic 5
zhlédnutí 2,2KPřed 2 lety
3 Body Problem Hamilton's Equations -&- Why View Motion in a Rotating Frame? | Topic 5
From Earth to Any Planet for FREE?
zhlédnutí 780Před 2 lety
From Earth to Any Planet for FREE?
3-Body Problem Lagrangian Equations and Effective Potential Energy | Topic 4
zhlédnutí 6KPřed 2 lety
3-Body Problem Lagrangian Equations and Effective Potential Energy | Topic 4
3-Body Problem Equations Derived, Part 2: Rotating Frame | Topic 3
zhlédnutí 3,4KPřed 2 lety
3-Body Problem Equations Derived, Part 2: Rotating Frame | Topic 3
3-Body Problem Equations Derived, Part 1: Inertial Frame and Non-dimensionalization | Topic 2
zhlédnutí 7KPřed 2 lety
3-Body Problem Equations Derived, Part 1: Inertial Frame and Non-dimensionalization | Topic 2
Three Body Problem Introduction: Lecture 1 of a Course Series | Topic 1
zhlédnutí 9KPřed 2 lety
Three Body Problem Introduction: Lecture 1 of a Course Series | Topic 1
How Microbes Cross the Air-Water Interface from Harmful Algal Blooms & the Water Cycle
zhlédnutí 176Před 2 lety
How Microbes Cross the Air-Water Interface from Harmful Algal Blooms & the Water Cycle
Vortex Ring and Air Mass Boundaries #shorts
zhlédnutí 265Před 2 lety
Vortex Ring and Air Mass Boundaries #shorts
Lagrangian Coherent Structures Introduction
zhlédnutí 2,8KPřed 2 lety
Lagrangian Coherent Structures Introduction

Komentáře

  • @aidancoletta7153
    @aidancoletta7153 Před 2 dny

    New to this idea and im tryna understand better: when you say that the lyapunov exponent is .9 for the Lorenz system, I'm a little confused. If you're closer to the trivial equilibrium point of the Lorenz system at <0, 0, 0>, shouldn't the lyapunov exponent be negative for some initial conditions?

    • @ProfessorRoss
      @ProfessorRoss Před dnem

      Great question. The Lyapunov exponent is independent of initial location; it's determined from following any initial condition for long enough. Even when you're near the equilibrium point at <0, 0, 0>, the dynamics will still take the state away from <0, 0, 0> zipping around, and eventually going onto the strange attractor, where it will wander chaotically forever. (I'm assuming we're talking about a parameter r in the regime where the strange attractor exists).

  • @alihosseiniroknabadi4828

    Thanks Professor

  • @alihosseiniroknabadi4828

    It was great

  • @Eta_Carinae__
    @Eta_Carinae__ Před 5 dny

    As I understand it, Hamilton kinda got his big break as a mathematician/physicist with the Hamiltonian, but as an alternate formalism, it wasn't well known at the time. Quaternions came afterward - which became the precursor for vector analysis, after Oliver Heaviside more or less invented the notion of a vector, which was essentially a quaternion, but instead of the relationship between i,j,k, he took the two parts of the product of quaternions - the scalar part and _the rest,_ i.e. the vector part - and just defined two operations that would return each part when applied to a vector.

  • @forheuristiclifeksh7836

    18:07

  • @forheuristiclifeksh7836

    1:45

  • @forheuristiclifeksh7836

    0:10 0:10

  • @statebased
    @statebased Před 6 dny

    Super content, but also tempo of presentation!

  • @Deepthinker4617
    @Deepthinker4617 Před 6 dny

    Sir, I have a doubt that has given me a headache. Sir, the non-linear dynamics and chaotic systems you talk about, these are higher level physics and maths concepts, right? I am in 11th grade; are we taught these concepts or not, or are we only taught about simple systems with some assumptions so that the system does not become chaotic, like assuming friction is not present or value of g is constant everywhere? Am I correct, sir?

  • @jarekk.8247
    @jarekk.8247 Před 7 dny

    The universe is probably a fractal on the largest scale with the number of dimensions equal to π.

  • @vacoff2717
    @vacoff2717 Před 7 dny

    great tutorial, enjoyed both 3 parts

  • @forheuristiclifeksh7836

    1:00

  • @forheuristiclifeksh7836

    1:00

  • @enriquealvarado3989

    Hi great video! Question -- is there transient chaos in the windows of periodicity after around r = 28, or is it only in that first region where we have two fixed points?

  • @phenixorbitall3917
    @phenixorbitall3917 Před 8 dny

    Nice!

  • @botondnagy7649
    @botondnagy7649 Před 8 dny

    Unfortunately the link with the Matlab code is dead...😕

    • @ProfessorRoss
      @ProfessorRoss Před 8 dny

      Try this link tinyurl.com/cr3bpmatlab And thanks for letting me know!

  • @forheuristiclifeksh7836

    30:15

  • @tabhashim3887
    @tabhashim3887 Před 9 dny

    Hello Dr. Ross, is the homework assignments you reference in the videos available?

  • @vacoff2717
    @vacoff2717 Před 10 dny

    this is utterly fucking great

  • @Musiclover5258
    @Musiclover5258 Před 14 dny

    Hi Prof. Ross, @38:00, is it implicitly assumed that the center of mass lies on the axis of rotation (omega)? If otherwise, the point G will itself be orbiting around the axis. Or, is the mathematical definition of angular momentum h_G applicable for any arbitrarily chosen body frame origin, whether it lies on the axis of rotation or not? I apologize if this had been discussed in an earlier lecture, in which case please advise - I had skipped a few. Thank you again for a great series.

  • @AtharvaPawar-j1x
    @AtharvaPawar-j1x Před 16 dny

    We can predict outcomes in this case , by applying physics laws😅

  • @MarkKrebs
    @MarkKrebs Před 16 dny

    I think you miss centripetal acceleration. Imagine the same dynamics, but you're swinging a dumbell on a string. Same stability applies. So the gg frequency should be faster. Gotta go study it a bit. Thoughts?

  • @ogunstega7348
    @ogunstega7348 Před 20 dny

    Hi Prof. at 13:31 what about trajectory that repeat it self after sometime but these trajectory are sensitive to initial conditions, would you call them periodic(because it does repeat) or chaotic (because of sensitivity to IC)? Thanks

  • @SujanDahal
    @SujanDahal Před 22 dny

    Thank you ❤ From Nepal

  • @Musiclover5258
    @Musiclover5258 Před 24 dny

    I have watched/listened to only lectures 12 and 13 in his series yet, but what a sheer joy to go through this material❤❤ Thank you Professor Shane Ross!! I have a quick question. Is this course at the undergraduate or graduate level? My son will be doing his Masters in Aerospace (he did his undergrad in Mechanical Engineering), and I am planning to urge him to go through your lecture series in its entirety beforehand. So, I was wondering if this material would be comfortable for him assuming that he starts from Lecture 1 - my background is EE from many years ago, hence I am unable to make this judgment. Are there prerequisites? Thank you.

    • @ProfessorRoss
      @ProfessorRoss Před 23 dny

      Thank you for the kind words! This course is a first semester graduate level course taken by students in mechanical and aerospace engineering. I've also taught a junior-level undergraduate version of it, but that has been discontinued. In terms of prerequisites, you should have previous experience with kinematics and dynamics (e.g., using Newton’s equations in an undergrad course), calculus and differential equations, and computational methods (e.g., using Matlab to solve ordinary differential equations and to visualize the solutions). And to be honest, to get the most out of this course, you should like math and dynamics.

    • @Musiclover5258
      @Musiclover5258 Před 23 dny

      @@ProfessorRoss Thank you Professor Ross, I appreciate the feedback. >> And to be honest, to get the most out of this course, you should like math and dynamics. I do, in fact I deeply love this stuff. Hoping that it will be hereditary🙂.

  • @khandmo
    @khandmo Před 26 dny

    Perfect explanations. A great teacher explains why, not what.

  • @drxkalishnakov2464
    @drxkalishnakov2464 Před 28 dny

    Incredible work doctor , the accompanying documentation youve put into your videos and referencing them all together into a cohesive course is invaluable. Much appreciation from a fellow aerospace engineer who needs a refresher on attitude dynamics once in a while. Do you happen to have a book published that might accompany this course and serve as a reference manual?

  • @telmanmaghrebi3358
    @telmanmaghrebi3358 Před měsícem

    This is like a GOD! Oh my God, Excellent!

  • @michaeln.8185
    @michaeln.8185 Před měsícem

    Thank you for making this available!

  • @russellthescout9639
    @russellthescout9639 Před měsícem

    you can see the distribution is skewed a bit

  • @caber007
    @caber007 Před měsícem

    A wonderful set of lectures! Thank you so much for your work.

  • @ramcharanthota1016
    @ramcharanthota1016 Před měsícem

    Thanks for great lecture, Professor. I need small clarification. In transport theorem, whether the velocity seen by B frame is expressed in B frame or E frame. If it is expressed B frame, how it is equal to velocity seen by E frame expressed in E frame

  • @jagadishkumarmr531
    @jagadishkumarmr531 Před měsícem

    I am an aerospace masters student trying to specialise in control & simulation and I think these lectures are one of the best! Helped me understand the kinematics and rotation matrices very well! Thanks a lot for these free content!

  • @cmancuso84
    @cmancuso84 Před měsícem

    In the far shots it doesn't look like the station is wobbling, but in the closer shots the station is actually wobbling from the view point of the smaller ship.

  • @sangjoonan2308
    @sangjoonan2308 Před měsícem

    Hi! I'm really enjoying your videos! It's really helpful with my studies. I'm wondering what kind of software did you use to plot vector field and see the behavior? Thank you

  • @coolmatt3906
    @coolmatt3906 Před měsícem

    Nice explanation! Also called EMA exponential moving average.

  • @annavasconcelos8698
    @annavasconcelos8698 Před měsícem

    Great content, professor!

  • @Karlemilstorm
    @Karlemilstorm Před měsícem

    0:25 "people are walking around"? Eh? 😁

    • @ProfessorRoss
      @ProfessorRoss Před měsícem

      Yeah, I guess I got that detail wrong 😆 You get it though, people bouncing off the walls causes small but significant torques on the spacecraft.

  • @bryanmendoza3694
    @bryanmendoza3694 Před měsícem

    Could you recommend a book that has examples of non-canonical Hamiltonian systems? Also theory. Thank you

    • @ProfessorRoss
      @ProfessorRoss Před měsícem

      I learned some examples from my PhD advisor Jerry Marsden, who wrote a book with Tudor Ratiu, "Introduction to Mechanics and Symmetry". This has several examples, but begins at a high level. Another book I've heard good things about is Darryl Holm's "Geometric Mechanics - Part I: Dynamics And Symmetry"

  • @eledwhenelaena9753
    @eledwhenelaena9753 Před měsícem

    It was really helpful. Thank you so much

  • @casey-gt8nl
    @casey-gt8nl Před měsícem

    Oh my gosh!! This is wonderful

  • @KenderGuy
    @KenderGuy Před měsícem

    I'm not seeing any Chinese scientists being protested or going insane or any weird VR devices or infinitely expanded protons How is this related to 3 Body Problem?

  • @sabari273
    @sabari273 Před měsícem

    gravity cause wobble .. in space i think no wobble

  • @Ivanovichx
    @Ivanovichx Před měsícem

    Thanks for the great video-series. I just have a question regarding the MATLAB Kalman filter using both data from the gyro and the accelerometer. If I understand it correctly, z is our measurement. Ignoring gravity, our measurement is omega_1, omega_2 and omega_3 given by the gyro. That is converted to quaternions to be able to write x_{k+1} = A * x_k where x is the state with the 4 quaternions. The kalman filter uses H as the matrix that maps states to measurements. With H = identity(4) means we're measuring directly the quaternions (I'm assuming because we can translate omega vector to quaternions. But when we incorporate the data from the accelerometer, I don't see how this fits into the Kalman filter. If I'm understanding the previous video correctly, we have two new measurements, meaning H should be a 6x6 matrix. Instead, the code seems to simply use roll and pitch obtained from the accelerometers as initial guesses rather than measurements. Could you clarify this? Thanks.

  • @freeman3467
    @freeman3467 Před měsícem

    You are great, man!

  • @Kurzy123
    @Kurzy123 Před měsícem

    That was great! I wasn't even looking for that content but I stayed because it was very well delivered and interesting! Thanks!

  • @StupidusMaximusTheFirst
    @StupidusMaximusTheFirst Před měsícem

    Really good and simple explanations of complicated stuff. Thanks.

  • @Dysiode
    @Dysiode Před 2 měsíci

    You know what I love? Constant pitch noise. Can't get enough of it. Honestly, it's astonishing more music isn't just one or two tones for 2:30-4:00 minutes. 0/10 thumbs down

    • @Dysiode
      @Dysiode Před 2 měsíci

      Also, you're holding the phone differently. I guess the "Dr." in your name wasn't for anything remotely scientific.

  • @3dindian
    @3dindian Před 2 měsíci

    Why around 4:05 it was mentioned that Lagranigian is not always T-V? Is it hinting at non-mechanical systems? 2nd question: At around 38:28, it is said that the kinetic energy T can be a function of T(q_i, q_idot). Can you point to a system where T has explicit dependence on q_i. Moreover, at 46:13, we write {\partial L \over \partial q_i} = -{\partial H \over \partial q_i}. If the kinetic energy is a function of q_i in a general case, then {\partial H \over \partial q_i} = - {\partial L \over \partial q_i} + \sum_{i=1}^{n} \dot{q}_i {\partial p_i \over \partial q_i}, where {\partial p_i \over \partial q_i} may not turn out to be zero. So my question essentially is: how is kinetic energy a function of position vector explicitly? Thank you for your time

    • @CrustyJoeMC
      @CrustyJoeMC Před měsícem

      For example, in polar coordinates, the r coordinate will appear in kinetic energy

  • @liku1716
    @liku1716 Před 2 měsíci

    I am 18 years old and don't know much about these filters, and wanted to make a drone, almost everything was easy but I just couldn't grasp this concept, I think I watched more than 10 videos on kalman filter, nothing got through. But then I found this video, it was really easy to understand. thank u professor for your good work

    • @ProfessorRoss
      @ProfessorRoss Před měsícem

      I'm glad I was able to help. I hope the drone project goes well!